Submarines and their Weapons - Aircraft of World War II

Roger Ford
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Page 2: Fieseler Fi 103s - Vis - line the corridor of an underground factory.

Contents
INTRODUCTION 6
CHAPTER ONE
JET AIRCRAFT 8
CHAPTER TWO
ROCKET-POWERED AIRCRAFT 34
CHAPTER THREE
HYBRID AIRCRAFT AND GLIDERS 44
CHAPTER FOUR
ROTARY-WING AIRCRAFT 52
CHAPTER FIVE
SURFACE-TO-SURFACE MISSILES 60
CHAPTER SIX
AIR-TO-AIR WEAPONS 84
CHAPTER SEVEN
AIR-TO-SURFACE MISSILES 90
CHAPTER EIGHT
SURFACE-TO-AIR MISSILES 100
CHAPTER NINE
ARTILLERY 108
CHAPTER TEN
TANKS AND ANTI-TANK WEAPONS 120
CHAPTER ELEVEN
SUBMARINES AND THEIR WEAPONS 128
CHAPTER TWELVE
NUCLEAR, BIOLOGICAL AND CHEMICAL WEAPONS 138
INDEX 142

Introduction
Before we begin to examine the large and diverse
array of secret weapons produced in Germany
before and during World War II, we should perhaps
define what is meant by the term 'secret'. Most
weapons are developed in secret - or at least, under
conditions of stringent security - whether in times of
peace or war, if only because, as the old adage has it,
forewarned is forearmed. In Germany's case, there
was an added imperative: the Versailles Treaty which,
at the end of World War I, forbade her to develop (and
even to possess) certain categories of weapons, such
as aircraft and tanks. Development programmes for
these weapons had to be carried out in absolute secrecy,
since the ultimate risk (though probably a small
one by the time these development programmes were
under way) was the occupation of Germany by the
victorious Allies. In many cases, up until the moment
that Hitler signalled his intention to revoke the Treaty
unilaterally, the projects were actually based outside
Germany: in Holland, the Soviet Union, Sweden and
in particular Switzerland.
In the strict sense, then, when we address the topic
of German secret weapons of World War II, we are
faced with an enormous task. But the term 'secret
weapons' has a more precise meaning in general use:
it implies something which goes beyond the development
of a piece of more or less mundane equipment
in conditions of secrecy. It implies a genuinely new
concept, something truly out of the ordinary, which
simply could not work without a new understanding
of physical science or chemistry; a new mastery of
technology; or some great leap of creative, imaginative
invention. In the place and at the time in question,
there was certainly no lack of those.
WUNDERWAFFEN
Perhaps the alternative term frequently used in Germany
at the time - Wunderwaffen - comes closer to
defining the true nature of these secret devices, for
they were often truly things of wonder, being either
completely new and hitherto undreamed-of outside a
small select group, or achieving previously unthinkable
levels of performance thanks to breakthrough
innovations in science and technology. Some of them,
it is true, were 'ideas whose time had come', in that
the basic principle was understood, but had not yet
been successfully applied, and in these cases, teams
of scientists and engineers in America, Britain and
Germany (and sometimes elsewhere: there were several
significant advances made by Italy) were engaged
in a headlong race to get the first reliable working version
onto the battlefield. The development of the jet
aircraft and of radar, not to mention the development
of nuclear fission, stand out amongst those. But in
other areas, particularly in rocketry and the invention
and perfection of the all-important guidance systems,
Germany stood head and shoulders above the rest.
Left: The Junkers Ju 287, with its forward-swept wings,
was just one of a number of futuristic designs developed
by German scientists and engineers in World War II.

Her scientists made an enormous and outstanding
contribution, not just to the German war effort, but to
modern civilisation. However, there were areas where
German science and technology were deficient, most
importantly - arguably - in the field of electronic
computing machines, which were not weapons themselves
but something without which the bounds of
technological development would soon be reached.
However, all too often these deficiencies arose as a
result of demand chasing insufficient resource, and
time simply ran out for the scientists of the Third
Reich before a satisfactory result could be produced.
TOO LITTLE, TOO LATE
Time and again in the course of this work we will
come upon development programmes which were
either cancelled before they came to fruition or which
were still in progress at the war's end. Many of them,
of course, did not get under way until 1944, when the
spectre of defeat was already looming large in Berlin
and many essential items were in increasingly short
supply. We can only speculate upon the possible outcome
of an earlier start on the course of the conflict.
Others were cancelled simply because they did not
appear to offer the likelihood of spectacular results,
and in those cases we can, all too often, detect the
hand of Adolf Hitler. In general, we can note what can
only be described as a wrong-headed insistence on his
part that big (and powerful) was always beautiful (and
irresistible). This major flaw led him to push for the
development of weapons such as the fearsome - but
only marginally effective and very expensive -
PzKpfw VI Tiger and King Tiger tanks, which would
have been far better consigned to the wastebin from
Above: A borderline secret weapon: the 'Goliath' was an
explosives-filled wire-guided tank and a typically
innovative approach to dealing with bunkers and armour.
the very outset, and the resources squandered upon
producing them - and then keeping them in service -
redirected into more appropriate channels such as the
more practical PzKpfw V Panther.
In a very real sense, Hitler himself motivated and
ran the German secret weapons programme. There
seems to be a direct and very tangible link between
this programme and his psyche, and we are perhaps
left wondering whether the Wunderwaffen would have
existed without him. On balance, it seems certain that
they would have done, given the creative imagination
of so many German scientists and the readiness of
many of her military men to accept innovation, but it
is equally certain that without Hitler's insistence,
many weapons systems which made a very real
impact upon the course of the war would either not
have been developed at all, or would, at best, have
been less prominent.
Nonetheless, without the genius of many German
scientists and the brilliance of German technologists
and engineers, the entire programme would have been
stillborn. Many of the weapons produced for the first
time in Germany and employed in World War II went
on to become accepted and very important parts of the
broader armoury, and several have made an enormous
impact on life as a whole outside the military arena.
The more spectacular failures have a certain grandeur,
despite their shortcomings, and even the outright
myths - and there were many, some remarkably persistent
- frequently had an underpinning of fact.

CHAPTER ONE
Jet Aircraft
Thrust-powered flight was an early alternative to the airscrew propeller - in 1928,
only a quarter century after the Wright brothers first took to the air, Fritz Stammer
flew in a rocket-powered glider. By the time a further decade had gone by, both
rocket- and jet-powered aircraft had become a reality, and a central plank in
Germany's attempts to win control in the air.
The German Air Force, the Luftwaffe, was held in
high esteem in National Socialist Party (henceforth,
Nazi) circles, and it perhaps enjoyed better
access to the ultimate seat of power, namely Adolf
Hitler, than the Army or the Navy. This was not just
because it had at its head one of the Fuhrer's closest
associates, Hermann Goring, but also because for
almost all of the war, it had sole charge of the frontline
defence of Germany against the combined
onslaughts of the British and American air forces,
bombing by night and by day.
Certainly, when it came to the allocation of funds
for research and development, the Luftwaffe was at
the head of the line; as a result, more developments
Above: The stark shape of the Messerschmitt Me 262.
Left: The Heinkel He 162 made use of appropriate
technology- in this case, plywood; its wing and tailplane
assemblies were manufactured in furniture factories.
were made in the field of aeronautics in the Third
Reich than in any other. That there was something
approaching chaos in the way individual projects
were initiated, approved and evaluated is a constant
source of wonder, because in a country which prided
itself on its logical, methodical approach to problemsolving,
there was no logic or method in evidence! As
one expert has commented, the relationship between
the individual aircraft and engine manufacturers and
also between them and the Luftwaffe and the Reichsluftfahrtministerium
(RLM - the German Air Ministry)
looked like tribal warfare.
Those projects which came to fruition were
amongst the better-known wartime developments,
and not just in Germany, but that only tells half, or far
less than half, the story. The vast majority fell by the
wayside, some due to lack of time; others, quite properly,
because they were flawed; still others because
they were simply too fanciful and apparently farfetched.
Most of the more interesting new aircraft

JET AIRCRAFT
developed during World War IT in Germany were to
be powered by either turbojet or rocket motors, in
both of which German scientists and engineers
excelled, but as we shall see, the jet engine programme
in particular was to get off to a very slow
start. Had the optimism of the jet pioneers been justified,
we might well have seen a different outcome to
the war, a prolongation, perhaps, into the autumn and
winter of 1945, which might have resulted in the
nuclear bombs used against Japan being dropped on
German cities, too. When it was so evident that the jet
aircraft was going to be so vitally important, it comes
as something of a surprise to see that the timescale of
its development was so extended. As a result,
although Germany had a very clear lead in the field,
she squandered it, thanks largely to poor overall control
of the research and development programme.
THEHEINKELHe178
The name Heinkel deserves to figure high in any list
of notable achievements in aviation, for it was from
Ernst Heinkel's design studio, and specifically from
the drawing boards of twin brothers Siegfried and
Walter Günter, that the first practical thrust-powered
aircraft - the rocket-propelled He 176 and the turbojet-powered
He 178 - were to come. Heinkel himself,
with partner Hellmuth Hirth, had enjoyed considerable
success with the Albatros aircraft, especially the
B.I, during World War I. He struggled through the
dark days of the 1920s and came to prominence again
with a commercial aircraft, the Giinter-designed He
70 and, using that as a stepping-stone, produced
arguably the most effective bomber of its day, the He
111, which first flew in early 1935. Heinkel continued
to develop successful piston-engined aircraft, but his
10
HEINKEL He 178
Type: Single-seat research aircraft
Length: 7.51 m (24.54ft)
Wing area: 7.90rri2 (85.04sq ft))
Max weight: 1990kg (4387lb)
interest also turned to the emerging technology of
rocketry. There had been thrust-powered flights -
Fritz Stammer flew a solid-fuel rocket-powered glider
for the first time on 11 June 1928 - but it took
almost a further decade and the development of liquid-fuelled
motors to make it a practical proposition,
as we shall discover in Chapter Two when we come to
examine rocket-propelled aircraft.
Rocket motors, while they could hardly be called
'tried and tested' by 1938, were simple in the
extreme; far more complicated, but offering huge
advantages in terms of fuel economy and controllability,
was the revolutionary new turbojet powerplant
on which Heinkel's engineer, Joachim Pabst von
Ohain, and his assistant Max Hahn, were working in
secret. Lured away from Göttingen University, where
they had done their pioneering work, the pair produced
a first demonstration prototype, the HeS 1,
which ran only on hydrogen (and was only barely
controllable) to produce about 250kg (55()lb) of static
thrust, in September 1937. By the time six more
months had passed, they had made considerable
progress, and had produced the petrol-fuelled HeS 3,
which developed 500kg (HOOlb) of thrust. This, they
believed, was a practical - if only marginally - powerplant,
and the next step was to produce an airframe
in which to mount it.
The result of their efforts was the He 178, the
world's first jet-propelled aircraft. It was a shoulderwing
monoplane with its cockpit well forward of the
wing leading edge, where it sat above the ducting
Below: The Heinkel He 178, despite its shortcomings, was
the first jet-powered aircraft to fly successfully, on 27
August 1939, 20 months before Britain's Gloster E.28/39.
Max speed: estimated 580km/h (360mph)
at sea level
Range: N/A
Armament: None

HEINKEL He 280
Type: Single-seat prototype interceptor
Length: 10.40m (34.125ft)
Span: 12.20m (40.00ft)
Max take-off weight: 4310kg (9502lb)
Max speed: 900km/h (560mph} at 6000m
(19,700ft)
which brought air to the engine (which, along with its
tailpipe, occupied most of the rest of the fuselage). It
made its first true flight on 27 August 1939, having
'hopped' along the runway three days earlier. This
pre-dated the maiden flight of the Gloster E.28/39,
powered by Frank Whittle's engine, which had in its
turn pre-dated Chain's original effort, by over 20
months. The He 178 was demonstrated to the RLM on
1 November. Almost incredibly, there was virtually
no official interest, and it (along with the He 176) was
consigned to the Berlin Air Museum, where both
were destroyed in an air raid in 1943.
THE HEINKEL He 280
Heinkel abandoned the He 178 largely because of
technical problems associated with mounting the
engine within the fuselage, but did not give up hope
of developing a turbojet-powered fighter. New blood
in the shape of Max Mueller arrived from Jumo to pep
up the jet engine development programme. He
worked on the the HeS 30, which became the 109-
006. The 109- prefix was employed, somewhat confusingly,
for both pulse-jet and turbojet engines and
also for rocket motors; the three-figure designator following
was allocated chronologically, and there is no
logical distinction between one manufacturer and
another. Thankfully, there were few enough engine
types, so one soon became familiar with the rather
impersonal system.
Simultaneous with Mueller's work was that of
Pabst von Ohain who developed the HeS 3 as the HeS
8 (109-001). Both engines were to be tested in an allnew
airframe, the He 280. This was a twin-engined
aircraft, its powerplants slung beneath the low wings
in nacelles and with a high tailplane with a fin and
Range: 650km (404 miles)
Armament: 3 x 20mm MG 151 cannon
Above: The second Heinkel jet, the He 280, was
successful, but lost out in competition with the
JET AIRCRAFT
M esse rsc h mitt Me 262. Just nine examples were built
rudder at each tip. It made its first powered flight with
von Ohain's engines on 2 April 1941, and was demonstrated
to the Luftwaffe and RLM three days later.
Now the reaction was different. The immediate
result was that Heinkel's engine division expanded in
size with the addition of his old partner Hirth's company
(which made piston engines and turbo-chargers
amongst other things). Mueller and his team moved to
the Hirth factory at Stuttgart, and von Ohain stayed at
Rostock-Marienehe to work on a further development
of his engine, the 109-011, which was projected to
give 1300kg (28661b) of static thrust. There was
understandable rivalry between the two teams and
both made considerable progress, but for some unaccountable
reason, the RLM decided to order work on
the 109-006 to be discontinued, even though it was
already producing 900kg (19841b) of thrust. Meanwhile,
development of the Oil continued at Stuttgart,
but even by the end of the war, it had never run except
on a test bench and just 20 had been completed. Testing
of the He 280 continued with both Jumo 004 and
BMW 003 engines, but when it eventually came up
against the Me 262, it fared badly. There are suggestions
that the decision to adopt the Me 262 was at
least partly politically motivated, since, as we have
noted, the relationship between the various German
planemakers themselves, and with the RLM and the
Luftwaffe, was a political minefield. The nine prototypes
constructed were later used for testing new
wing and tail designs and Heinkel later worked on
other jet aircraft designs, most of them centred on the
11

JET AIRCRAFT
stillborn Oil engine, but none came to fruition until
the submission which became the He 162 (qv) was
accepted.
THE Me 262 'SCHWALBE/STURMVOGEL
The best known of the aviation projects which actually
came to fruition is the Messerschmitt Me 262, the
aircraft chosen over the He 280. By modern standards,
this was a fairly conventional all-metal fighter
aircraft with gently swept low-set variable-chord
wings, powered by twin Junkers Jumo 004B-1 turbojet
engines. It became the first jet-powered aircraft to
enter operational service, on 3 October 1944, and was
thus a landmark in aviation history. We shall examine
the development history of the Me 262 in more detail
than other aircraft, both because it was so significant
and because it will give us an insight into the methodology
of aircraft development in the Third Reich,
revealing that it was by no means a smooth process.
The Me 262 started life as a loosely defined project
of the RLM, inaugurated in 1938, with Hans Mauch
and Helmut Schlep working on the powerplant and
Hans Antz on the airframe. Schlep, recently returned
from college in the United States, had already convinced
Junkers Motorenwerke (Jumo - the engine
division of the forcibly nationalised planemaker) to
start work on designs for axial-flow turbojets, and
BMW, initially sub-contracted by Junkers, had also
begun to develop a more sophisticated design of its
own. In the meantime, Antz had interested Messerschmitt's
chief of development, Robert Lusser, in
examining the possibilities of producing an airframe
to carry such a powerplant. Before the end of the year,
the project had moved up a gear, and Messerschmitt
1 2
Above: A pre-production version of the Me 262 gets
airborne with the help of solid-fuel rocket motors. Such
'RATO' (Rocket-Assisted Take-Off) units were widely used
to assist heavily loaded aircraft into the air.
Below: In all, some 1430 Me 262s were to be produced in
seven different variants. This bomber variant, the Me
262A-2a 'Sturmvogel', was operated by KG 51 out of
Prague-Ruzyn in late 1944.
MESSERSCHMITT Me 262A-2a/Ul
Type: Single-seat bomber
Length: 10.61 m (34.79ft)
Span: 12.50m (41.01ft)
Max take-off weight: 6775kg (14,936lb)
Max speed: 870km/h (541 mph) at 7000m (23,000ft)
Range: 845km (525 miles)
Armament: 2 x 30mm MK 108 cannon;
1000kg (2200lb)bombload

was instructed, somewhat baldly, to begin development
work on a fighter aircraft which was to have an
endurance of one hour at 850km/h (530mph).
Responsibility was placed in the hands of Woldemar
Voigt (of whom more later), who examined both single-
and twin-engined arrangements before concluding
that a single centrally mounted engine layout
would present more problems than it would solve. His
view was coloured by the performance of the He 178.
Instead Voigt suggested a design with engines in each
wing root, which crystallised into Project 1065 in
Messerschmitt's Augsburg design office. Detailed
design drawings were produced as early as 7 June
1939, and a wooden mock-up then made. On 3 March
1940 Messerschmitt was awarded a contract to produce
three airframes, designated as the Me 262, for
flight testing.
It was envisioned that the aircraft's power would
come from two BMW P.3302 engines, delivery of
which had been promised for the end of 1939, and
their non-appearance was only the first of a long
series of setbacks associated with the powerplant. In
fact, the prototype BMW engine, now known as the
109-003, did not run until August 1940, and then it
produced only 150kg (3301b) of static thrust instead
of the 600kg (13201b) promised. A year later it was
JET AIRCRAFT
still only producing 450kg (9901b), which was by no
means enough to get the Me 262 into the air. It was to
be mid-1943 before an 003 engine produced sufficient
power to be viable, and a further year before production
units became available, and in due course it was
decided to reserve it for the Heinkel He 162 (see
below). In addition, the BMW engine had proven too
big to fit into the wing-root mount, and the design
team had hurriedly modified the Me 262 to carry it in
under-wing nacelles, though this, in turn, simplified
main spar design. Some sources suggest that this factor,
not the diameter of the BMW engines, underlay
the decision to adopt nacelles rather than faired-in
mountings, even at the expense of increased drag.
FIRST ALL-JET Me 262 FLIGHT
The Jumo 109-004 was always to have been a less
sophisticated design, sacrificing ultimate potential for
a 'fast track' into production. It, too, had its problems,
however. The prototype ran in November 1940, but it
was January 1942 before all the snags were ironed
out, and its first flight, slung under a Messerschmitt
Bf 110, took place on 15 March. The first pilot-production
engines, 004As, which produced 840kg
(185()lb) of static thrust, were rolled out in early summer,
and were fitted to the Me 262 V3, which made

JET AIRCRAFT
the first all-jet Me 262 flight on 18 July 1942 in the
hands of Fritz Wendel. The aircraft had flown as early
as 18 April 1941, but with a single 1200bhp Jumo
210G piston engine in its nose, and by that time an
aircraft which was ultimately to be its closest competitor,
the Heinkel He 280 (qv), had already flown on
the power of two 500kg- (HOOlb-) thrust HeS 8 turbojcts.
Orders for 15 Me 262s were placed, expanded
to 60 by early October, by which time the second prototype
had also flown, and the first Jumo 004B
engines, with similar performance characteristics to
the -As, were going into production.
PROPELLED BY AN ANGEL
On 22 April 1943, Adolf Galland, the operational
head of the Luftwaffe, flew the aircraft himself (and
returned to say it felt 'as if an angel were pushing
me'), and was instrumental in convincing the RLM to
switch most of Messerschmitt's production from the
Bf 109 to the Me 262, the formal order for general
production being issued on 5 June. On 26 June the
production prototype, -V5, with a nosewheel undercarriage,
took to the air. A blow fell on 17 August
1943: production of the Me 262 was just getting into
Below: The two-seater Me 262B-1 was normally
employed as a night-fighter, but these aircraft lacked the
distinctive 'toasting-fork' antenna on the nose, which,
incidentally, slowed the night-fighter down.
14
full swing when the USAAF bombed the Messerschmitt
factory at Regensburg, destroying much
important tooling. The company's development programmes
were transferred from Augsburg to Oberammergau
as a result, with further attendant delays. By
November, the future looked less bleak, with prototypes
flying with pressurised cockpits and carrying
armament (the as yet imperfect MG 108 30mm cannon)
and with Junkers finally getting the 004B engine
into series production, but then another quite different
problem arose in the shape of direct interference from
the Führer himself.
Senior Luftwaffe personnel, aware that they were
losing the fight to limit the success of the RAF and
USAAF bombing campaign, had begun to advocate
that the production of bomber aircraft in the Third
Reich should cease and that all efforts should concentrate
on fighter types. Goring agreed, but Hitler
recoiled at the very suggestion and would have none
of it. Instead, he decided that the Me 262 would be
perfect to carry a 500kg (11 OOlb) bombload to England
to continue his pet campaign of harassment and
nuisance raids, and he ordered the aircraft to be modified
and developed for this purpose alone, even
though it was hardly suitable and no adequate bombsight
was available, nor was one ever produced.
It was May 1944 before Hitler agreed to allow production
of the 'Schwalbe' ('Swallow') fighter version
to continue, and then only in parallel with the

Above: This Me 262A, 'White 10' (the distinctive markings
are largely obscured), was flown by Leutnant Kurt Bell of
III/EJG 2 during the making of a Luftwaffe training film.
Note the aircraft's pristine appearance.
'Sturmvogel' ('Storm Petrel') bomber, at the rate of
one fighter to 20 bombers. Furthermore it was 4
November before he gave permission for it to go into
unlimited production. By then, 13 pre-production Me
262A-Os had been completed, in addition to 12 development
prototypes, and 60 more were scheduled to
roll out during the following month. There was still
much 'fine tuning' to be done, and versions of the aircraft,
both bombers and fighters, were testing in a
variety of forms, but more importantly, pilot training
had begun. It was still to be five months before the Me
262 was ready to go to war, but essentially by mid-
1944 the development emphasis had switched from
Messerschmitt to the Luftwaffe, although the firm
was still heavily involved, developing the two-seater
trainer and night-fighter versions, as well as alternative
forms for the stillborn hochgeschwindigkeits (HG
- high speed) version.
MESSERSCHMITT Me 262B-la/Ul
Type: Two-seat night-fighter
Length: 11.53m (37.83ft)
Span: 12.48m (40.96ft)
Max take-off weight: 6585kg (14,515lb)
JET AIRCRAFT
In the final analysis, the Me 262 was simply too little,
too late. The German jet scored its first confirmed
combat victory in the hands of Leutnant Joachim
Weber - his victim was a PR XVI Mosquito of No.
540 Squadron, RAF - on 8 August 1944, four days
after the British Gloster 'Meteor' Mk 1 had made its
combat debut (though admittedly, the latter's debut
'victory' had been over a pilotless VI (lying bomb).
That bare statistic is a telling indictment, for the
British had not flown their prototype jet aircraft, the
E.28/39, until almost 21 months after Heinkel's He
178 had taken to the air.
Me 262 VICTORIES
Some 1430 Me 262s were to be produced, in seven
main versions, but probably no more than a third of
them actually saw combat (and over 100 were lost,
many in accidents on landing) over a seven-month
period. By the spring of 1945 they were operating
under very difficult circumstances but were still
downing American bombers in significant numbers,
particularly when equipped with 5.5cm R4M 'Orkan'
('Hurricane') unguided rocket projectiles, despite a
never-cured tendency to snake at high speed, which
made aiming somewhat unpredictable. The total number
of victories scored by Me 262s is uncertain, but is
authoritatively put at more than 735. The highestscoring
pilot was Oberleutnant Kurt Welter, with over
20 victories, and 27 other Luftwaffe pilots became jet
aces, with five or more victories each, including
Below: The Me 262B-1 night-fighters of 10/NJG 11 were
assigned to the defence of Berlin. One of the unit's pilots,
Feldwebel Karl-Heinz Becker, accounted for seven Allied
aircraft. Note the radar array on the nose.
Max speed: 813km/h (505mph) at 6000m
(19,700ft)
Range: 1050km (652 miles)
Armament: 4 x MK 108 30mm cannon
15

JET AIRCRAFT
Messerschmitt Me 262A-1a
cutaway drawing key
1. Flettner-type geared trim tab
2. Mass-balanced rudder
3. Rudder post
4. Tail fin structure
5. Tailplane structure
6. Rudder tab mechanism
7. Flettner-type servo tab
8. Starboard elevator
9. Rear navigation light
10. Rudder linkage
11. Elevator linkage
12. Tailplane adjustment
mechanism
13. Fuselage break point
14. Fuselage construction
15. Control runs
16. FuG 25a loop antenna (IFF)
17. Automatic compass
18. Aft auxiliary self-sealing fuel
tank (600 litres; 132 gallons)
19. FuG16zyR/T
20. Fuel filler cap
21. Aft cockpit glazing
22. Armoured aft main fuel tank
(900 litres; 198 gallons)
23. Inner cockpit shell
24. Pilot's seat
25. Canopy jettison lever
26. Armoured (15mm; 0.6in]
head rest
Generalleutnant Adolf Galland, who formed and then
commanded the ad hoc unit known as 'Jagdverband
T after being implicated in the January 1945 'revolt'
of Luftwaffe fighter unit leaders.
Was the Messerschmitt Me 262 worth the time and
effort it took to develop, when all was said and done?
The answer is a qualified 'yes', but the situation, most
16
27. Canopy (hinged to starboard)
28. Canopy lock
29. Bar-mounted Revi 16B sight
(for both cannon and R4M
rockets)
30. Armourglass windscreen
(90mm)
- 31. Instrument panel
32. Rudder pedal
33. Armoured forward main fuel
tank (900 litres; 198 gallons)
34. Fuel filler cap
35. Underwing wooden rack
for 12 R4M 5.5cm
rockets
36. Port outer flap section
37. Frise-type aileron
38. Aileron control linkage
39. Port navigation light
40. Pitothead
41. Automatic leading-edge slats
42. Port engine cowling
43. Electrical firing mechanism
44. Firewall
45. Spent cartridge ejector chutes
46. Four 30mm Rheinmetall-Borsig
MK 108 cannon (100 rpg beltfed
ammunition for upper pair
and 80 rpg for lower pair)
47. Cannon muzzles
48. Combat camera
49. Camera aperture
50. Nosewheel fairing
51. Nosewheel leg
52. Nosewheel
53. Torque scissors
54. Retraction jack
55. Hydraulic lines
56. Main nosewheel door (star-
board)
57. Compressed air bottles
58. Forward auxiliary fuel tank (170
litres; 37 gallons)
59. Mainwheel well
60. Torque box
61. Main spar
62. Mainwheel leg pivot point
experts agree, would have been very different had the
two major hold-ups - the late delivery of the engines
and the Fuhrer's meddling - been somehow speedily
dealt with. Had the Luftwaffe's fighter squadrons
been able to operate it in significant numbers from,
let's say, mid-1944, the outcome would probably have
been very different. Tt would not have won the war for

63. Mainwheel door
64. Mainwheel retraction rod
65. Engine support arch
66. Leading-edge slat structure
67. Auxiliaries gearbox
68. Annular oil tank
69. Riedel starter motor housing
70. Engine air intake
71. Hinged cowling section
72. Junkers Jumo 004B-2 axial-flow
turbojet
73. Starboard mainwheel
74. Wing structure
75. Automatic leading-edge slats
76. Main spar
77. Starboard navigation light
78. Frise-type ailerons
79. Trim tab
80. Flettner-type geared tab
81. Starboard outer flap section
82. Engine exhaust orifice
83. Engine support bearer
84. Starboard inner flap structure
85. Faired wing root
Germany, but it might well have prolonged it by some
months by making inroads into the Allies' (especially
the Americans') strategic bombing campaign, thus
helping to maintain German manufacturing production
levels. The question of whether that would have
been a good or a bad thing lies outside the scope of
this work.
JET AIRCRAFT
Left: Despite its revolutionary wing form, the Me 262 was
constructed along entirely conventional lines, the only
limiting factor of the powerplant being the need to keep
the airframe components out of the exhaust stream.
THE Ar 234 'BLITZ'
The only other jet-propelled German aircraft to see
serious combat during World War II came not from
one of the major manufacturers, but from a relatively
minor player. Prior to the development of the Ar 234
'Blitz' ('Lightning') bomber (also known as the
'Hecht' - 'Pike'), the Arado company had only ever
been involved in the production of light aircraft.
Many of them, such as the Ar 196, were produced as
floatplanes, designed to operate from warships,
though that is not to say that its products were anything
less than excellent. In 1940, the RLM issued a
specification for a high-speed reconnaissance aircraft
to be powered by two jet engines, either Jumo 004s or
BMW 003s. Arado responded with a design - the
E.370 - for a shoulder-wing monoplane with engines
in under-slung nacelles, which was accepted as the Ar
234. Two prototypes were constructed over the winter
of 1941-42, but it was February 1943 before the first
pair of engines, the Jumo 004Bs, were delivered, and
15 June before the aircraft first flew. It was entirely
conventional for the period, save in one respect: the
fuselage was very slim and instead of a wheeled
undercarriage, it used a take-off trolley and landed on
skids. This was clearly unacceptable in an operational
aircraft since it made manoeuvring on the ground next
to impossible, so midway through the prototype programme,
the fuselage was marginally widened
beneath the wings, and main wheels and a retractable
nosewheel were installed. Arado engineers also developed
a rocket-powered interceptor, the E.381, which
was to have been carried as a parasite beneath the
fuselage of the Ar 234. Nothing came of the idea.
Most of the early Ar 234s were completed as
reconnaissance aircraft, and flew many successful
missions at 700km/h (435mph) at between 9000m
(29,530ft) and 12,000m (41,000ft), where they were
largely immune to attack, but a bomber version with
either one or two seats, and able to carry 2000kg
(4400lb) of bombs, was also produced. It was February
1945 before the first of these aircraft, assigned to
KG 76, were operational. One was shot down by
American P-47 Thunderbolts near Segelsdorf on 24
February, and fell into Allied hands. The most important
missions KG 76 undertook were those aimed at
the destruction of the Ludendorff Bridge over the

JET AIRCRAFT

Rhine at Remagen between 7 and 17 March, when Ar
234s made repeated and often suicidal attacks supported
by Me 262 bombers of KG 51. A night-fighter
version of the Ar 234 was produced in small numbers,
and operated from March 1945 with some success.
Later Ar 234 variants had a variety of different powerplants,
and a four-engined version using 'siamesed'
nacelles was also produced in prototype. Maximum
speed at medium level of the latter was over 850km/h
(530mph), which was beyond the level-flight capabilities
of any Allied fighter, but still by no means fast
enough for absolute safety. The limiting factor on its
performance was not, however, the engines: it was the
design of the wing. Straight wings have a finite maximum
speed, after which compression causes local
airflow to exceed the speed of sound, resulting in
potentially catastrophic instability. Arado's engineers
discovered this the hard way, but soon designer
Riidinger Kosin came up with an alternative planform:
a crescent wing, starting out with its leading
edge sweeping back from the wing roots, the curve
returning so that the wingtip sections were at rightangles
to the body axis (a form which was later used
in the British Handley-Page 'Victor' bomber). Wind
tunnel tests showed this to be much more effective,
but the war ended before a prototype could be constructed.
And even while the Ar 234 was in development,
engineers elsewhere were looking at much
more advanced concepts.
Left: The Arado Ar 234 - this is the production-B variant -
with its long, slim fuselage and wings, was the only real
alternative to the Me 262, but was nowhere near as
successful in operational terms.
ARADO Ar 234B-2
Type: Single-seat tactical light bomber
Length: 12.64m (41.46ft)
Span: 14.44m (46.29ft)
Max take-off weight: 9800kg (21,605lb)
THE JUNKERS Ju 287
JET AIRCRAFT
There is no space here to go into the complex aerodynamics
of wing form in any depth, save to say that as
early as the mid-1930s, it had been accepted - following
the work of the Deutsches Versuchsanstalt für
Luftfahrt (DVL - the German Aviation Development
Establishment) - that straight wings had a finite speed
limit thanks to the rise in drag caused by air compressing
at their leading edge. As we have seen, this
was the main factor in limiting the speed of the Ar
234. An interim solution was to sweep the leading
edge backwards but keep the trailing edge straight,
thus producing a variable-chord wing, and this was
adopted with piston- and jet-engined aircraft alike.
The Me 262 had a wing essentially of this form
(although it did have a small sweep to its trailing edge
outboard of the engines) as did the altogether more
pedestrian Douglas C-47/DC-3 transport. At this
time, no aircraft had flown with a wing that had
steeply swept leading and trailing edges, even though
it was known from wind tunnel testing that such a
wing would benefit not only from decreased compressibility
but also from a reduction in the ratio
between its thickness and its chord (the distance
between the leading and trailing edges).
In June 1943, at about the time when the Arado Ar
234 first flew, a development team at Junkers, under
Dr Hans Wocke, produced a design for an advanced
bomber using a double-swept wing form, but with one
Below: A total of 210 examples of the Arado Ar 234B were
produced; just one remains, on display in the Smithsonian
Institution's National Air and Space Museum in
Washington D.C.
Max speed: 742km/h (461 mph) at 6000m
(19,700ft)
Range: 1630km (1013 miles)
Armament: 2 x 20mm machine guns
(some aircraft); 2000kg (4400lb)
bombload

JET AIRCRAFT
Above: Surrounded by Junkers Ju 88Gs, this Ar 234B was
captured by US forces at Manching in Bavaria in April
1945. The state of its cockpit bears out the assertion that
the full glazing offered no protection against flying debris.
further innovation. The wing was to be swept not
back, but forward, conferring all the advantages outlined
above but also resulting in greater stability,
except under certain well-defined circumstances.
Wocke's project was championed by Siegfried
Kneymeyer who was already a leading advocate of
the abandonment of all piston-engined aircraft manufacture
(save for the Junkers Ju 88) in the Reich.
A CHANGE AT THE TOP
In November 1943, Kneymeyer took over from Ernst
Udet as Chief of Technical Air Armament at the
RLM, and thus had considerable influence. The following
March, prototype development of Wocke's
new aircraft, designated the Ju 287, was ordered, and
construction of a flying testbed began, using the fuselage
of a Heinkel He 117. It was to be powered by

Above: The Ar 234B was found to be underpowered, and
the obvious solution was to double up on the powerplants
to produce the Ar 234C. Both reconnaissance and nightfighter
versions were built alongside the bomber variant.
four 004B engines of 900kg (19841b) thrust each, two
suspended from the wings, the other two mounted on
the fuselage sides, just below and aft of the cockpit. It
would have two Walter 501 rockets to assist take-off.
The prototype aircraft made its maiden flight on 16
August and proved to be predictable in flight, though
wing flexing was more of a problem than had been
anticipated and when it yawed the trailing wing tend-
JET AIRCRAFT
ed to lift and create a rolling moment. On the whole,
however, results were positive, and work went ahead
on the construction of a second prototype with a purpose-built
fuselage, to be powered by six BMW 003
turbojets, four wing-mounted and two mounted on the
fuselage. In July, however, a new Führerdirectiv instigated
the Reichsverteidigungs programme, which
ordered all development work not concerned with
Below: An early Ar 234 screeches down the runway as it
lands on its skids. Such a landing arrangement was out of
the question for operational purposes, so the fuselage
was widened and main wheels and a nosewheel fitted.

JET AIRCRAFT
Above: The Junkers Ju 287, with its forward-swept wings
and nose-mounted engines, was one of the more radical
aircraft of World War II. This is the sole example built, the
-V1 prototype. It was later captured by Soviet troops.
fighters and interceptors to be stopped, and accordingly
no further progress was made with the Ju 287
V2, though the Ju 287 VI continued to fly occasional
tests. Tn March 1945, the project was suddenly
revived and the Ju 287 ordered into production. Construction
of the Ju 287 V2 recommenced, and plans
were made for a -V3, with a pressurised three-man
cockpit, 4000kg (88001b) bombload, and remotely
controlled guns, to be powered by four Heinkel Oil
engines of 1300kg (28661b) thrust. Two Jumo 012
engines of 2780kg (61201b) thrust or two BMW 018
engines of 3400kg (74801b) thrust (neither of which
had actually been completed) were posited as an alternative.
Both the Ju 287 VI and the still-incomplete
-V2 fell into Soviet hands in May 1945; the former
was flown as found, while the latter was completed
with swept-back wings and is said to have achieved
speeds of around 1000km/h (620mph). Hans Wocke
later produced a civil aircraft, the HFB 320 'Hansa',
with a swept-forward wing.
THE He 162 'SPATZ'/'SALAMANDER'
By 1944, with the situation looking increasingly
black for Germany, there was a vocal school of
thought which advocated the development of almost
disposable weapons, to be used, in the last resort, by
barely trained personnel. Rather more practical was a
design which Heinkel produced in response to an
RLM requirement for the Volksjäger (People's Fighter),
a cheap and expendable fighter aircraft weighing
less than 2000kg (44001b), to be powered by a single
BMW 003 jet engine, with an endurance of 30 minutes
and an armament of two 30mm cannon. This
craft was to be flown by volunteers from the Hitlerjugend.
Design studies were 'invited' from Arado,

Blohm & Voss, Focke-Wulf, Junkers, Heinkel and
Messerschmitt on 8 September 1944, to be considered
a week later; the prototype aircraft was to fly before
the year's end.
Only Messerschmitt declined the invitation. The
Blohm & Voss design (P.211) was considered the
best, but for some reason, the Heinkel submission
(P. 1073) was chosen, placing the engine in a nacelle
mounted atop the fuselage; the engine discharged its
exhaust between twin rudders, and by that means
avoided all the problems of intake and exhaust ducting.
By 23 September, a mock-up had been built and
work began on the prototype the following day (six
days before an official order was delivered). By 29
October a set of final drawings had been produced.
Almost amazingly, the prototype flew for the first
time on 6 December - three weeks before the deadline
- but on a second flight on 10 December it
crashed during a high-speed low-level pass, killing its
pilot, Flugkapitän Peters, when the starboard wing
disintegrated. It was later discovered that a fault in the
formulation of the phenolic resin used to bond the
plywood from which the wings were fabricated had
caused the failure.
By the year's end, a variety of faults in stability
had shown up in the second prototype, though these
were all cured by mid-January (even if only to the
point where an experienced pilot could fly the aircraft;
it was still very much of a handful for a novice,
though the same was true of the Me 262). By the end
of the month, weapons' testing had shown that it
would be necessary to replace the 30mm MK 108
with the 20mm MK 151. With that, the Heinkel 162
'Spatz' ('Sparrow', as it was called within the firm; it
HEINKEL He 162
Type: Single-seat interceptor fighter
Length: 9.05m (29.71ft)
Span: 7.20m (23.625ft)
Max take-off weight: 2700kg (5952lb)
JET AIRCRAFT
Above: The Heinkel He 162, the 'People's Fighter', was to
have been operated by barely trained volunteers from the
ranks of the Hitler Youth, but it proved very difficult to fly.
later became known semi-officially as the 'Salamander')
went into production at most of the existing
Junkers and Heinkel factories (where the duralumin
semi-monocoque fuselage was constructed) and in
small furniture factories, where the wings and tail
assemblies were produced. Final assembly took place
at the Heinkel works at Rostock-Marienehe, at the
Junkers works at Bernburg, and at the vast underground
factory of 'Mittelwerke GmbH' near Nordhausen.
Once again, it was too late, of course, though
some 275 aircraft were actually completed and
around 800 more were ready for assembly. The Volksjäger
rarely saw combat, though it was claimed that
Below: The He 162A was straight winged, but designs
were drawn up for a version with swept-back wings and
another with forward-swept wings. Neither was built.
Max speed: 835km/h (519mph) at 6000m (19,700ft)
Range: 1000km (620 miles)
Armament: 2 x 30mm M K 108 or
2 x 20mm MG 151 cannon

JET AIRCRAFT
one aircraft - in the hands of Leutnant Rudolf Schmitt
of 1/JG 1 based at Leek near the Danish border in
Schleswig-Holstein - did shoot down a low-flying
RAF Typhoon on 4 May 1945 (the claim was not
allowed; the credit went to a nearby flak unit instead)
and one was shot down, killing the pilot. Nine other
members of JG 1 died and five were injured in flying
accidents during conversion from the Fw 190; the He
162 was still very unforgiving. Post-war evaluation by
Allied air forces indicated that with a little more
development work, it would have been entirely
viable, however, and would almost certainly have
made a considerable impact, if only it had been available
12 - or even 6 - months earlier.
THE EMERGENCY FIGHTER PROGRAMME
Expedients like the Volksjäger were not the only
option under consideration in mid-1944. It was
becoming increasingly obvious to the Luftwaffe's
Below: He 162 components were manufactured all over
Germany and sent to three central locations for assembly.
In all, some 275 aircraft were completed, and components
for around 800 more were on hand at the war's end.

High Command that it had effectively missed the
boat, and that the jet and rocket-powered fighters
which were about to enter service would soon be ineffective
against a new generation of Allied aircraft
such as the B-29 Superfortress with its 11,000m
(36000ft) plus ceiling. Just before the end of the year,
Kneymeyer issued a specification for a new generation
fighter to all the principal producers, with the
stipulation that the aircraft should be powered by the
HeS Oil engine. Roughly, the performance parameters
were a top speed in-level flight of around
1000km/h (620mph) at 7000m (23,00()ft) and a ceiling
of 14,000m (45,900ft); it was to be armed with
fourMK 108 30mm cannon. By February 1945, three
proposals had been received from Messerschmitt, two
from Focke-Wulf and one each from Blohm & Voss,
Heinkel and Junkers. On the last day of the month, a
selection committee sat and chose Focke-Wulf's Project
T to go into development as the Ta 183.
THE FOCKE-WULF Ta 183
The two projects from Kurt Tank's design department
were the work of a man who has been described as the
most important aerodynamicist in Germany at the
time, Hans Multhopp. They were essentially similar
in character: a fuselage which was no more than a
shroud for the single engine, its intake duct and
exhaust tube, with the pressurised cockpit and
weaponry sited above it, which was to be supported
on stubby swept-back shoulder wings (constant-chord
in Project I, variable-chord in Project II), with a tail
unit cantilevered out behind. The tail unit itself was
the factor which differentiated the designs. That of
Project I was entirely innovatory: a T-tail, with the
horizontal control surfaces located at its upper end;
that of Project II was conventional, with the tailplane
located low down. Otherwise, considerable attention
was paid to ease of manufacture with the sort of
resources which could be expected to be available,
and the result of that was a projection that each aircraft
would require a total of 2500 man-hours (the Me
262 probably never got far below 10,000). No single
Ta 183 was ever built, Focke-Wulf's factories having
been overrun by late April, but it is widely held that
the Soviet Army took a complete set of plans, and the
design team of Mikoyan and Gurevich is said to have
used them as the basis for the MiG-15, powered by a
Russian copy of the British Rolls-Royce 'Nene' turbojet
engine. SAAB in Sweden later produced a very
similar-looking aircraft as its SAAB-29, this time
powered by a copy of the de Havilland 'Ghost'.
THE MESSERSCHMITT P. 1101
JET AIRCRAFT
Another of the aircraft entered for the Emergency
Fighter Competition was also to form the basis of a
type built elsewhere, but this time rather more openly.
The Messerschmitt company had in fact anticipated
the need for a replacement for the Me 262 (who was
in a better position to know that aircraft's limitations?)
and construction of a prototype to replace it,
designed by Woldemar Voigt, had begun in July 1944
as the P. 1101. This was in one particular a remarkable
aircraft, for it was constructed chiefly to determine
the best angle of wing sweep; its variable-chord
wings could be reset (on the ground, not in flight) to
any angle between 35 and 45 degrees. Otherwise, the
aircraft was conventional in the new mould, with a
single engine located deep within the fuselage and
exhausting below the extension boom which supported
the tail assembly.
The prototype was about 80 per cent complete
when it was discovered by the Americans on their
arrival in Oberammergau, and it was put on display in
the open along with other 'interesting' developments
from the Messerschmitt studio. It was still there, deteriorating
rapidly, when it was spotted by Robert
Woods, Chief Designer at Bell Aircraft, who contrived
to have it sent it to the United States, where it
was eventually restored and completed, with the help
of Voigt himself, as a non-flying mock-up. It formed
the basis for the first ever variablc-geometry-winged
aircraft, the Bell X-5, the sweep angle of which could
be changed in flight to one of three pre-sets: 20, 40
and 60 degrees. This aircraft made its first flight on 20
June 1951, the geometry of the wing being varied in
flight for the first time on 15 July.
THE MESSERSCHMITT P. 1110 AND P. 1111
The other two submissions Messerschmitt made were
less well developed but somewhat more radical. The
P. 11 10 did away with the nose air intake, locating the
engine much further back in the airframe, with the
duct openings on the fuselage shoulders, just forward
of the trailing edges of the constant-chord swept
wings. The P. 1111 was more adventurous: an allwing
design of near-delta planform with a heavily
swept tail fin and rudder, the air intakes of which were
located in the forward part of the wing roots. A proposal
submitted too late for the competition was a
variant of this design, with a wing of narrower chord
and a butterfly tail. Under ideal circumstances, all
three designs would probably have been built in prototype
form and flown against each other, but as it
25

JET AIRCRAFT
DORNIER Do 335
Type: Single-seat fighter-bomber
Length: 13.85m (45.44ft)
Span: 13.80m (45.28ft)
Take-off weight: 9600kg (21,164lb)
was, none ever progressed beyond a partially completed
wooden mock-up.
THE OTHER CONTENDERS
The other submissions to the Emergency Fighter
Competition were all tailless designs too, which goes
to show, perhaps, how far that concept had been
accepted in Germany by the end of 1944. Of these
designs, Blohm & Voss's P. 212 was perhaps the most
radical, with twin stubby fins and rudders at the
wingtips, supporting a winglet - half a tailplane,in
fact - the rear surfaces of which formed elevators and
also acted as additional ailerons. Like all Blohm &
Voss's late wartime designs, the P. 212 was the work
of the Director of Development, Dr Richard Vogt,
who is credited with something like 200 different
ideas for new aircraft, virtually none of which even
made it to prototype. The design Heinkel submitted as
P. 1078C was for a more straightforward flying wing.
The wing itself was to have had considerable
anhedral, with the tips turned down through 40
degrees over their last 5()cm (20in) or so.
The Junkers P. 128 had a more conventional wing
planform, wider but with a narrower aspect-ratio and
set at shoulder height, although it had its engine
intake ducts located under the wing at about halfway
through their chord length. It had fin lets with rudders,
located about halfway between wing root and
wingtip, which protruded both above and below the
wing surface. All this was the work of Heinrich Hertel,
a comparative newcomer to Junkers who, until
1939, had worked with Heinkel on the He 176 and the
He 178. He left Heinkel largely, we are told, because
he had little faith in rocket power, so it was somewhat
26
Max speed: 765km/h (475mph) at 6500m
(21,325ft)
Range: 2060km (1280 miles}
Armament: 1 x30mm MK 103 cannon; 2 x
15mm MG 151 machine guns
Above: Besides its 30mm forward-firing cannon and 15mm
machine guns, the Do 335 could carry a 1000kg (2200lb)
bombload, half in its weapons bay and half on hardpoints
situated beneath its wings.
ironic that he was given the job of re-designing the
Me 163 'Komet' (qv) to produce the Ju 248.
Cursory though this analysis has been, we have
touched upon all the major German aircraft manufacturers
save two: Dornier and Henschel. Claudius
Dornier was, if anything, more conservative than even
Tank or Hugo Junkers, and would have nothing to do
with jet propulsion. His main contribution to aviation
innovation lay in his development of a twin-engined
fighter-bomber with its powerplants in a single axis:
Below: The Dornier Do 335 'Pfeil' was potentially the
fastest piston-engined aircraft ever built, with one
1800bhp Daimler-Benz DB 603 engine in the nose and
another in the tail.

one in the nose, driving a tractor propeller; the other
in the tail, driving a pusher. The Do 335 'Pfeil'
('Arrow', known unofficially as the 'Ameisenbär' -
'Anteater') was potentially the fastest piston-engined
aircraft ever built, yet still exhibited most of the
manoeuvrability of a single-engined fighter. It
showed no bad manners when flying on only one
engine, and could even take off with one inoperative.
The only drawback to the arrangement was that it
required special measures to abandon the aircraft in
an emergency. The rear propeller and upper tail fin
were jettisoned, then the canopy was blown off before
the pilot could attempt to bale out (though at least one
example was fitted with an ejection seat, the first in
operational service). Initially, there was considerable
resistance to its development from the RLM for the
somewhat inconclusive reason that Dornier built not
fighters but bombers, and the company had to under-
JET AIRCRAFT
Above: Total production of the 'Pfeil' ('Arrow'} remained
small, butthat did not prevent the German Air Ministry
from ordering prototypes in configurations to satisfy a
variety of roles.
take to build an intruder version before permission to
continue with the project was forthcoming. The first
prototype made its maiden flight in September 1943,
powered by two ISOOhp DB 603 engines. By the end
of the war, a version with 2100hp engines was flying.
Several proposals were in process of consideration at
the war's end, including swapping the rear engine for
an HeS 011 turbojet and linking two aircraft together
by means of a short central wing section, like the
Heinkel He 111Z 'Zwilling' (Twin'; see Chapter
Three). Henschel's most important work was to be
done in the Held of guided weapons, though the company
did propose a turbojet-powered dive-bomber,
97

JET AIRCRAFT
Above: Despite its appearance, the Heinkel He 177 was
actually a four-engined bomber - each nacelle housed a
pair of Daimler-Benz DB 601 engines, each producing
1000bhp, linked to a single propeller.
the Hs 132, which was very well received by RLM. It
was somewhat similar in form to the He 162, with a
single turbojet mounted in a nacelle above the fuselage
and a similar tail assembly (the similarities were
not accidental), with a narrow-diameter cigar-shaped
fuselage just big enough to accept a pilot in the prone
position. The company also worked on a contender
for the Emergency Fighter Competition, the Hs 135,
with a compound delta wing like that later incorporated
into the SAAB 'Draken'.
THE GERMAN HEAVY BOMBERS
Of course, jet and rocket engines powered only a
small minority of the new aircraft produced in Germany
during World War II. Most of them had 'conventional'
piston engines, but the development of
these aircraft, too, was far from smooth. During the
first three years of the war, at least, German aeroengine
manufacturers failed to come up with really
powerful piston engines and that caused airframe
designers to adopt some quite novel solutions to the
problem of attaining high performance levels, both in
fighter aircraft and in the elusive heavy/strategic
bomber development programme.
28
Even though the Luftwaffe was a tactical, closesupport
air force, there was a programme aimed at
developing a strategic bomber during the early years
of the Third Reich. This resulted in the development
of aircraft such as the Junkers Ju 89/Ju 90 and the
stillborn Dornier Do 19, but it died with the Luftwaffe
Chief of Staff, General Wever, in a plane crash on 3
June 1936, and was not resurrected until halfway
through World War II. Even at that relatively late date,
there was no suitable powerplant available for aircraft
capable of carrying a 2000kg (44001b) bombload to a
target 1600km (1000 miles) away at a speed of
500km/h (310mph), and the solution adopted was to
couple two engines together to turn a single propeller.
The choice fell on the lOOObhp DB 601, linked to
form the DB 606 (and later variants had more power,
culminating in the DB 613, which had 3600hp available
for take-off, with water injection and emergency
boost). It was a far from satisfactory solution, and for
a long time, the 'siamesed' engines tended to overheat
and first vaporise and then ignite petrol in adjacent
fuel tanks, with disastrous results.
Both the most important heavy bomber projects -
the Heinkel He 177 'Greif ('Griffon') and the
Junkers Ju 288C - had pairs of siamesed engines as
their powerplant. They were designed to carry both
conventional bombloads in internal bays and external
racks but also guided glider bombs such as the 'Fritz-
X' or the Henschel Hs 293 (see Chapter Seven); odd

suggestions for the Ju 288C included some other,
more outlandish features, such as fitting it with the
Düsenkanone 280 or the Gerät 104 'Munchhausen',
single-shot guns of 28cm and 35.5cm calibre respectively
(see Chapter Six). The Ju 388, which had even
better performance, was planned as both a heavy
bomber and a bomber destroyer, using Hs 298 and
Ruhrstahl X-4 guided air-to-air missiles, and was also
to have been employed in towing the Me 328 pulsejet-boosted
glider fighter to operational altitude. The
only one built in significant numbers was the He 177,
over 1000 of which were produced. One was modified
to carry the German atomic bomb and many were fitted
with forward-firing 5cm and 7.5cm anti-tank guns
to be deployed on the Eastern Front. However, it was
never entirely successful, even after five years of
development. The Ju 288 did not get past the prototype
stage. Some 65 Ju 388s of all types were built.
A high-altitude reconnaissance version of the He
177 was developed, powered by four (separate) DB
610 engines of 1750hp and with a new high aspectratio
wing and a new twin fin tail. Known as the He
274, the prototype was built in Paris at the old Farman
works, which were overrun in July 1944 before it
could be completed. It was finished by the French and
Below: The sole example of the Me 264, the original
'Amerikabomber', first flew in December 1942. Such close
attention was paid to its aerodynamic properties that the
joints in the wings and fuselage were filled with putty.
JET AIRCRAFT
Above: Like so many German aircraft projects, the He 177
was a case of 'too little, too late'. By the time it was ready
to go into production, the Luftwaffe had little chance of
operating a strategic bomber with any degree of success.
flown from December 1945. An improved version of
the bomber, also with four separate engines and a
twin fin tail, was built as the He 277, but only eight
were completed before the Emergency Fighter Programme
was put into effect on 3 July 1944.
THE'AMERIKABOMBER'
Although they were developed in considerable secrecy,
these aircraft do not really meet our criteria for
secret weapons, though some 'conventional' piston-

JET AIRCRAFT
engined bombers do. The Luftwaffe, we may recall,
was intended as a tactical, rather than a strategic, air
force, unlike the USAAF and the RAF, and it never
operated really large, long-range bomber aircraft, like
the American B-17 Flying Fortress or B-24 Liberator,
or the British Lancaster, in any substantial numbers. It
had aircraft, like the Focke-Wulf FW 200 'Condor'
and the Junkers Ju 290 (though the former was
designed as a civilian airliner and the latter was a
hasty transformation of another), which were capable
of flying very long distances, but these were intended
primarily for ultra-long-range maritime reconnaissance,
and while they did carry bombs (and variants
of both carried glider bombs), they were unsuitable
for use in combat conditions. Thus, when the USA
declared war on Germany in December 1941, the
Luftwaffe found itself without the means of attacking
its new-found enemy, and the RLM immediately
issued a specification for a suitable aircraft.
Three companies responded: Focke-Wulf with the
Ta 400; Messerschmitt with the Me 264; and Junkers
with the Ju 390. The Ta 400 was never built; the latter,
which was little more than a Ju 290 stretched in
wings and fuselage with two more engines, was reasonably
straightforward, and the first prototype flew
in August 1943. The second protype had a still longer
fuselage and carried FuG 200 Hohentweil search
radar and five 20mm cannon. On a test flight from
Mont de Marsan on the Atlantic coast of France, near
Bordeaux, it once approached to within 20km (12.4
miles) of New York before returning safely to base,
thus validating the operational concept. A third prototype,
this time a version able to carry 1800kg (39701b)
of bombs, was begun but never completed.
In fact, certain individuals at the RLM had begun
to contemplate the possibility of bombing New York
long before the United States entered the war, and
Willy Messerschmitt for one had begun to think about
a design for a suitable aircraft. His company was thus
well placed to satisfy the requirement when it was
issued in December 1941, and the prototype Me 264
made its first flight just 12 months later. With enough
fuel to reach New York and return safely (a flight of
anything up to 30 hours!), it could carry 3000kg
(66001b) of bombs, and still had enough capacity to
carry 1000kg (22001b) of armour plating. It had two
complete three-man crews with a sleeping area and
galley, and an elaborate defensive armament of four
13mm machine guns and two 20mm cannon. Under
overload conditions, the aircraft could be fitted with
up to six solid fuel rockets to assist it to take off. A
3 n
bewildering array of variants and variations were suggested,
including one to tow an Me 328 glider fighter
for protection, and another which would have been
the flying testbed for a steam turbine powerplant. Two
prototypes were begun; the first was destroyed in an
air raid just as it was about to begin ground tests, but
the second was completed and flew, being allocated to
Transportstaffel 5, which operated other large aircraft
types in the transport role. A version with greater
wingspan and six engines was contemplated, but
never produced. Thus the first round of the 'Amerikabomber'
contest made no more than a token impact,
but there was to be a second, as we shall see.
THE '3x1000' BOMBERS
Focke-Wulf, which produced the best German pistonengined
single-seater fighter-bomber of the war, the
Fw 190, had a genius in its Technical Director, Kurt
Tank, but a very conservative one. As a result, the
company was a latecomer to jet propulsion; too late,
indeed, to see any Focke-Wulf jet fly in other than
prototype form. One of those jets - the Fw Ta 183
(qv) - was to prove to be very influential indeed to
post-war development. In 1943, however, the company
did produce a series of designs to an in-house
requirement known as '3x1000' for an aircraft to
deliver a 1000kg (22001b) bombload to a target
1000km (620 miles) away at a speed of 1000km/h
(620mph). The first two designs had swept wings, one
of variable chord and one of fixed chord, and a conventional
tail assembly, but the third, which was much
more radical in nature, was for a tailless 'flying wing',
and shows very clearly the influence of Alexander
Lippisch, who acted as a consultant to Tank from time
to time. None of the designs was ever realised.
Messerschmitt proposed a design to meet the same
requirement, the P. 1107, which had moderately
swept-back wings and a butterfly tail. Two basically
similar designs were projected, the second of them
with much greater range, but neither was realised.
THE HORTEN BROTHERS
The second of those two aircraft, the P. 1107B, would
probably never have had trans-Atlantic range, but during
the plan's currency the prospect of bombing the
United States - which was now heavily involved in
the war against Germany, on the ground in Italy and
in the air from bases in the UK - reared up again.
Once again, design proposals for an appropriate aircraft
were solicited; this time a very different profile
emerged, and one which shows just how far aerody-

namics had progressed in Germany. The three main
contenders were all of delta wing planform, which
was clearly emerging as the shape of things to come,
either with or without vertical tail surfaces. Alexander
Lippisch was by no means alone in advocating it: the
Horten brothers, Walter and Reimar, were just as
committed and had been producing flying examples
of delta wing aircraft, both gliders and powered aircraft,
since the early 1930s.
The Mortens' first glider had been a wide delta,
with its leading edge swept back at 24 degrees and its
trailing edge straight, but the Ho II had its trailing
edges swept back, too. Four examples of the latter
JET AIRCRAFT
Above: The first prototype of the Horten Ho IX was
completed as a glider, but the second was fitted with twin
Jumo 004B engines and logged speeds in excess of
800krn/h (SOOmph). The Ho IX became the Gotha Go 229.
were built as gliders, and then one was fitted with a
6()hp Hirth motor driving a pusher propeller. Thanks
to Walter Morten's friendship with Ernst Udet, the
Luftwaffe procurement chief, this was put through a
quasi-official trial at the hands of one of the bestrespected
test pilots of the day, Hanna Reitsch. She
reported that its handling characteristics were
favourable, that it was not vulnerable to spin or stall,

JET AIRCRAFT
Above: Gotha engineers had misgivings about the ultimate
stability of the Go 229, and planned to halt the programme.
They were overtaken by events, however, and produced
only one prototype, with four more under construction.
but that it was not very manoeuvrable. A series of
designs, each better executed and more radical than
the last (and each of them tailless), followed, and by
the time of the Ho V, power had become the norm. By
1940, the Hortcns were operating a Luftwaffe design
studio known as 'Sonderkommando 9' at Göttingen,
and soon produced plans for the Ho VIII (a 60-seat
transport aircraft, powered by six pusher propellers),
and the Ho IX, a turbojet fighter with twin Jumo 004B
engines. The first prototype of the latter was completed
as a glider, and the second as a powered aircraft. It
was destroyed in an enforced single-engine landing,
but not before it had logged speeds in excess of
800km/h (500mph). It was to go into production as
the Gotha Go 229, with four MK 103 30mm cannon
and a 1000kg (22001b) bombload. Only one prototype,
with the more powerful Jumo 004C engine, was
completed before the war's end, though four more
were begun. Calculations suggest that the Go 229
would have had a top speed of over 1000km/h
(620mph) and indeed, it was presented to Hermann
Goring as a contender for the '3x1000' project, but
engineers at Gothaer Waggonfabrik were far from
happy with its straight-line stability as it had a tendency
to 'Dutch roll', yawing around the vertical Z
axis while rolling from side to side around the X axis.
The engineers planned to halt construction after the
sixth prototype. The Hortens agreed, and produced a
new design with a very pronounced, almost exaggerated,
V-shaped fin, the leading edge of which came
almost to the nose and included the cockpit. Lippisch

HORTEN Ho IX (GOTHA Go 229)
Type: Single-seat fighter-bomber
Length: 7.47m (24.51ft)
Span: 16.78m (55.05ft)
Max take-off weight: 8500kg (18,740lb)
Above: The Ho IX/Go 229 would probably have been
Max speed (projected): 1000km/h (620mph) at 6100m (20,015ft)
Range: N/A
capable of speeds in level flight in excess of 1000km/h
(620mph), which would have made it by far the fastest
production aircraft of its day.
Armament (projected): 4 x 30mm MK 103 cannon; 2000kg
(4400lb) bombload
produced several very similar designs. But the Hortens
did not give up the tailless concept either, and also
produced for a single-engine interceptor, though by
the time they reached the third evolution, this, too,
had become a delta with a conventional fin tail.
RE-ENTER THE 'AMERIKABOMBER'
By the time the Ho IX/Go 229 project was underway,
the RLM had resurrected the 'Amerikabomber' programme,
but the planemakers selected - Arado,
Focke-Wulf, Heinkel, Junkers and Messerschmitt -
had made little progress. Siegfried Kneymeyer then
contacted the Hortens and asked them to turn their
attention to a bomber with trans-Atlantic range. Not
surprisingly, they came up with a flying wing, essentially
an enlarged Ho IX, which they called the P. 18.
All the would-be contenders were summoned to a
conference at the RLM in February 1945, and the
Horten design was selected for production. The brothers
were instructed to work with designers from
Junkers and Messerschmitt, but the proposed consortium
soon fell apart when more conservative elements
insisted on adding a large fin and hinged rudder to the
design. Reimar Horten then went directly to Goring
with a modified plan for the P. 18B, employing four
HeS 011 engines in place of six Jumo 004s or BMW
003s, saving 1000kg (22001b) with little loss of thrust.
The aircraft, he confidently predicted, would have a
JET AIRCRAFT
range of 11,000km (6835 miles) at 850km/h (530
mph) and fly at an altitude of 16,000m (52,500ft) with
a 4000kg (88001b) bombload. He was told to go ahead
and build it, but by that time the war had only 10
weeks to run and it is doubtful whether detailed plans
were drawn up, though they may have been later, as
both brothers continued to work in aviation for the
rest of their lives, Walter eventually becoming a leading
light in the new Luftwaffe, Reimar in the aircraft
industry in Argentina.
THE JUNKERS P. 130/P. 140
Junkers had, in addition to Hans Wocke, two other
extremely talented designers in Ernst Zindel and
Heinrich Hertel. These three soon responded to the
new-found interest in all-wing aircraft and proposed
one such of their own as Project 130. It is suggested
that Hertel had produced the Ju 287 design only as a
means of gaining experience in the sort of aerodynamics
required by the P. 130, but it is worth bearing
in mind that he had acquired some relevant experience
with the Ju 322 (see Chapter Three). Similar in
character to the Hortens' P. 18B, the P. 130 had a
shorter range (around 5800km; 3600 miles), and was
apparently intended to operate against targets in Soviet
Asia and in England from bases in Prussia. The
'committee-modified' version of the P. 18A, with the
addition of the long triangular tail fin, became the
Junkers P. 140, with the range to carry 4.06 tonnes (4
tons) of bombs to New York. Like the P. 18B, it was
ordered into production, but work had hardly begun
before the underground factory in the Harz mountains
where it was to have been built was overrun.

CHAPTER TWO
Rocket-powered
Aircraft
Rocket-propelled interceptor aircraft were very attractive to the German Air Ministry,
for they seemed to offer a realistic possibility of being able to threaten the high-flying
Allied bombers which, by 1944, were decimating the country's industrial base. This
was particularly true since they did not require fossil fuel, which was in very short
supply by that time, and could be constructed cheaply, largely from plywood; a
considerable effort was put into developing such aircraft, but ultimately to no avail.
Had we been considering the history of thrustpowered
flight in something like chronological
order, rather than in terms of the impact the new technology
had on the course of aviation in World War IT,
we would have examined the rocket before the jet. In
fact, there is little conflict here, for the first effective
demonstrations of the two types occurred almost
simultaneously and in the same place: in the last
months before the outbreak of war, at Ernst Heinkel's
factory at Rostock-Marienehe. While neither type was
actually conceived as a weapons platform, and even
Above: The Messerschmitt Me 163B-1 'Komet'.
Left: The Ba 349 had four solid-fuel booster rockets and a
liquid fuel sustainer motor, Launched vertically, it was to
have climbed to 14,000m (45,900ft) in one minute.
though neither did what was hoped of it, thanks to a
series of poor design decisions, both demand inclusion
here because of the influence - both positive and
negative - they exerted. We have seen how the jetpropelled
He 178 was deficient because its designer
failed to solve the problem of how to induct air to the
engine efficiently. This, it must be said, would have
been hard to foresee. The main fault of the rocketpowered
He 176, on. the other hand, was glaringly
obvious, at least to the cognoscenti. Unfortunately,
there were few of them around in 1939.
THEHEINKELHe176
The rocket-propelled aircraft designated the He 176
by the Reichsluftfahrtministerium (RLM - the German
Air Ministry) was powered by a Walter Rl motor
3fi

ROCKET-POWERED AIRCRAFT
using hydrogen peroxide. Earlier versions (more
accurately, existing He 112 fighters with auxiliary
motors) had used a power unit developed by Wernher
von Braun (qv), which used liquid oxygen and alcohol,
a rather more volatile mixture. The near-explosive
decomposition of hydrogen peroxide into superheated
steam when it comes into contact with a catalyst
such as calcium, potassium or sodium permanganate
was to become a mainstay of German propulsion
programmes in a number of very different areas,
as we shall see. The He 176 flew for the first time on
30 June 1939. The aircraft probably never exceeded
the standard it had been designed to beat, 700km/h
(435mph), which was below the world speed record
of the day. It was essentially too heavy both for its
powerplant and for its short, stubby wings. The RLM
showed little interest in it, favouring the design which
would become the Messerschmitt Me 163 'Komet'
(qv). Heinkel abandoned the project.
ALEXANDER LIPPISCH
Alexander Lippisch was a self-taught aerodynamicist
who had worked at Zeppelin/Dornier after World War
1, then at Rhön-Rossitten-Gesellschaft (RRG - which
Below: The Messerschmitt Me 163 'Komet' interceptor
first went into action in August 1944. It accounted for only
about a dozen Allied bombers in six or seven months.
developed gliders for meteorological research,
amongst other things), and later, when RRG was
absorbed into it, at the Deutsches Forschungsinstitut
für Segelflug (DFS - German Glider Research Institute).
Lippisch maintained that had Heinkel had even
a narrow understanding of the nature of gliders, he
would have realised that he needed a large wing area
(and a small wing loading) to make an aircraft such as
the He 176 fly adequately, as it had only very
marginal power reserves. Instead, Heinkel had given
his proto-rocket aircraft short, stubby wings which
were really little more than control surfaces, and his
experiments failed in direct consequence. Lippisch
went further than that, of course. Like the Horten
brothers, he was a staunch and unremitting advocate
of the tailless, delta-pianform flying wing, and was
the first to fly such a design, in 1931. Three years
before that, however, Lippisch had produced a rocketpropelled
glider for automobile manufacturer Fritz
von Opel, who saw the new technology mostly in
terms of its ability to attract crowds, but who was
interested enough (and rich enough) to provide seed
money for would-be pioneers. Opel lost interest in the
early 1930s, after rocket-powered gliders had been
the death of a number of pilots. Lippisch's 'Ente'
('Duck') became the first rocket-powered aircraft to
fly, with Fritz Stammer at the controls, on 11 June
1928. By 1933, Lippisch had designed a variety of

MESSERSCHMITT Me 163B-1
Type: Single-seat interceptor fighter
Length: 5.69m (18.66ft)
Span: 9.33m (30.60ft)
Max take-off weight: 4110kg (9061 Ib)
delta-wing gliders and had begun to fit small engines
to them. He collaborated with Focke-Wulf and with
Gerhard Fieseler, and with the latter, built the twoseat,
twin-engine (pusher and tractor) Delta III
'Wespe' ('Wasp') and Delta IV, only to see both crash
at the cost of one pilot's life within a fortnight. RLM
promptly banned tailless aircraft, and it was some
time, and then only at the urging of Professor Walter
Georgii, the Director of DPS, before the ban was lifted.
A modified Delta IVb followed, with the RLM
designation DPS 39, and in 1939, orders were issued
for the construction of a version to be powered by a
Walter rocket motor. DPS built the wings, which were
of near-delta planform, and Heinkel built the rest of
the airframe, alongside the He 176 with which it
shared its powerplant. The design's concession to the
RLM was the small wingtip rudders, but after windtunnel
testing, Lippisch concluded that these would
only cause flutter and, ultimately, main spar failure.
Thus, the DPS 194, its successor, acquired a single,
central fin and rudder. Using as its 'fuel' T-Stoff (an
80 per cent aqueous solution of hydrogen peroxide
plus oxyquinoline as a stabiliser) and Z-Stoff (an
aqueous solution of sodium and potassium permanganates
to promote decomposition), the Walter RI-
203 rocket was to propel the prototype at speeds of up
to 500km/h (310mph). It was clear from the outset
that this was a major achievement and Lippisch was
ordered to Messerschmitt's Augsburg research centre
with his research and development team in January
1939. There the DPS 194 metamorphosed into the
Messerschmitt Me 163 'Komet' ('Comet').
ROCKET-POWERED AIRCRAFT
Above: 'White 13' - an Me 163B-1a of 1/JG 400, which
operated from near Leipzig between July 1944 and April
1945, defending the Leuna-Merseburg refinery complex.
THE Me 163'KOMET'
The 'Komet', which preceded the jet-propelled Me
262 into service by a little over two months, was a
radical and adventurous approach to the problem of
how to defeat the heavily armed and protected
bomber aircraft which were flown in formations
designed to create an impenetrable defensive box. Its
designation, all of them were decided by the RLM, is
somewhat misleading, for Messerschmitt AG actually
had little to do with its development, which remained
in the hands of its creator. In the spring of 1941, the
prototype of the new aircraft began gliding trials;
towed to a height of up to 8000m (26,250ft), it was
soon achieving speeds of up to 850km/h (530mph)
while retaining a high degree of controllability, and
during the summer it was sent to the rocket development
establishment at Peenemiinde-West on the
Baltic coast, to be fitted with a rocket motor - an
improved model of the Walter Rl incorporating a
degree of thrust control but still using T-Stoff and Z-
Stoff as its fuel. The development programme at
Peenemünde was fraught with accidents, some fatal,
as time after time the volatile fuels spontaneously
exploded. On one occasion, an entire building was
demolished. However, it also resulted in the Me 163
VI breaking the world speed record repeatedly until
the test pilot, Heini Dittmar, finally exceeded
1000km/h (620mph), almost killing himself in the
37

ROCKET-POWERED AIRCRAFT
FIESELER Fi 103R REICHENBERG IV
Type: Single-seat flying bomb
Length: 8.00m (26.25ft)
Span: 5.715m (18.75ft)
Launch weight: 2180kg (4806lb)
Above: The Reichenberg IV, as the manned version of the
VI flying bomb was known, was little more than a fantasy,
though prototypes did fly.
process when the aircraft became suddenly uncontrollable
as compression shock (shocks caused by airflow
over the wing surface locally exceeding the speed of
sound) induced negative lift and massive vibration. In
the event, Dittmar managed to regain control and land
successfully. The RLM, impressed, ordered prototypes
of an operational aircraft, the Me 163B, to be
armed with a pair of MG 151 20mm cannon and powered
by a more powerful 509-A2 rocket motor using
the somewhat less unpredictable combination of T-
Stoff and C-Stoff (30 per cent hydrazine hydrate, 57
per cent methanol, 13 per cent water) as its fuel and
producing 1500kg (33001b) of thrust. Around 2.032
tonnes (2 tons) of propellant (very nearly half the
entire weight of the aircraft) was enough to take it to
its operational ceiling of 12,100m (39,700ft) in 3.35
minutes, and the pilot then had a further four and a
Max speed: 650km/h (404mph) at sea level
Endurance: 20 minutes
Payload: 850kg (1874lb) warhead
half minutes of powered flight available: thus, he
would actually have been gliding, unpowered, during
most of his mission.
Two Me 163B-las were handed over to a special
Luftwaffe unit early in 1943 to allow pilot familiarisation
to begin, though it was July before training
actually commenced. The high landing speed of the
'Komet' (around 220km/h; 140mph) combined with
the fact that the pilot was committed to it from the
outset, having no power available to allow him to
regain height for a second attempt, resulted in many
accidents, most of them fatal. The first operational
unit, equipped with Me 163B-la aircraft, with a pair
of 30mm cannon in the wing roots and a considerable
degree of armour protection for the pilot, began forming
at Wittmundhaven in May 1944, and first went
into action as 1/JG400 on 16 August. It scored its first
success some days later, when Leutnant Hartmut Ryll
downed a B-17 near Leipzig. In all, some 300 Me
163s in various versions were constructed (and rights
to it were sold to Japan, where five powered and over

50 unpowered versions were built before the war's
end), but the aircraft was only a very limited success,
accounting, it is believed, for little more than 12
American B-17s. An improved version, known originally
as the Ju 248, was produced at Junkers and then
taken over by Messerschmitt as the Me 263. It was
somewhat larger, had a wheeled undercarriage rather
than skids, and was powered by a Walter 509C motor.
It was produced in prototype form only.
THE SELBSTOPFERMÄNNER FIGHTERS
In fact, like the Me 262, the 'Komet' was too little, too
late. So desperate was the situation in Germany by the
summer of 1944 that individual fighter pilots had
taken to ramming Allied bombers, and units such as
IV/JG3 and TI/JG300 were formed as Sturmgruppen
(assault groups) with that as an accepted fall-back tactic
using Fw 190A-8/R2s fitted with frontal armour.
They had a measure of success: between 7 July 1944
and the end of March 1945, when they ceased to operate,
they accounted for around 500 Allied bombers,
but only 10 of them by ramming. In April 1945, Sonderkommando
Elbe was formed from volunteers; they
trained for 10 days in ramming tactics, and then went
into action. In all, they rammed and downed eight, but
at a high cost to themselves: a total of 77 Bf 109s and
Fw 190s. If such potentially self-sacrificial Selb-
Stopfermänner tactics were to be employed, then
clearly a much less sophisticated aircraft, using little
in the way of strategic materials, could be employed
instead of some of the best piston-engined fighters of
the entire period.
At this point we need to take a very short diversion
to consider the nature of Selbstopfermänner tactics. It
was never the stated intention to require or even ask
aircrew to commit suicide in Germany in the way that
it was in Japan, and great pains were taken to maintain
that the very reverse was actually the case. The
Selbstopfermänner were expected only to employ
their aircraft as weapons in the last resort (though
recruits to the Sturmgruppen were required to take an
oath that they would indeed do this if necessary), and
to make every effort to ensure that the attack left them
with the possibility of escape. As will be noted when
discussing the manned Fi 103s, the possibilities of
this happening were remote, and it must be concluded
that there was a secret agenda, and that the men
Right: The launch of the Ba 349 was so violent that the
pilot was expected to black out; the climb to operational
altitude was under a simple automatic guidance system.
ROCKET-POWERED AIRCRAFT
(and women; Hanna Reitsch was an advocate of such
tactics) concerned knew exactly what they were being
called upon to do, and that the disclaimers were there
only for public relations purposes.
THE Ba 349'NATTER'
The 'Komet' was hardly a sophisticated aircraft.
However, according to Dr Erich Bachern the 'Komet'
was over-sophisticated. Bachern was an experienced
glider pilot and one-time Technical Director of Fieseler
AG, which was latterly a manufacturer of wings for
Henschel missiles and control surfaces for the A4 and
where Bachem had designed the Fi 156 'Storch'
('Stork') observation and light utility aircraft. He
claimed that a wooden glider, simple enough to have
been built in a carpentry workshop and propelled by a
similar rocket motor to that used in the 'Komet',
39

ROCKET-POWERED AIRCRAFT
BACHEM Ba 349
Type: Single-seat expendable interceptor
Length: 6.10m (20.00ft)
Span: 3.60m (11.81ft)
Launch weight: 2200kg (4850lb)
Above: The 'Natter' was conceived as the simplest means
of getting a man within range of the high-flying bombers.
The array of rockets in the nose were its sole weapons.
aided by four solid-fuel boosters so that it could take
off vertically, would do the job equally well. It would
climb to 14,000m (45,900ft) in little over a minute
under control of a simple automatic guidance system,
whereupon its pilot, by now hopefully having
regained consciousness after blacking out under the
forces generated at take-off, would take over and
4fl
Max speed: 800km/h (500mph) at sea level
Radius of action: 40km (25 miles)
Armament: 24 Föhn 7.3cm (2.8in) rockets
make a diving attack on the enemy bomber formation
on his way back to earth. He would bale out to land
by parachute only when he had fired his only armament
(the 24 Henschel Hs 217 'Föhn' 7.3cm or R4M
5.5cm unguided rockets contained in an array in the
nose), and had reduced his speed to around 250km/h
(155mph), while the 'aircraft' from the cockpit back
also descended by parachute in the hope of recovering
the rocket motor for re-use. From 22 December 1944,
a series of 11 unmanned launches were made on the
power of the booster motors alone, and on 23

February 1945, a single, unmanned test launch took
place using the Walter motor as well. Some days later
a manned launch was ordered by the SS
(Schutzstaffeln: the Nazis' private army) which, by
that time, had control of all secret weapons projects,
even though the unmanned programme had not been
completed and there were grave doubts about the aircraft's
viability. The pilot, one Lothar Siebert, was
killed when the Ba 349 power-dived into the ground
from a height of 1500m (4900ft) after having rolled
on to its back. The testing programme continued, and
perhaps 20 aircraft (some reports say 36) intended for
operations were produced, but none flew in combat. It
is thought that two examples remain, both in museum
storage: one in the USA, the other in Germany.
Ernst Heinkel proposed a very similar aircraft to
the Bachern 'Natter' ('Viper'). The P. 1077 'Julia' (it
never received an RLM designator) was also to have
been powered by a Walter 509 motor and four solidfuel
Schmidding 533 boosters. It was to have taken
off from an inclined ramp, to climb to 15,000m
(49,210ft) in 72 seconds, and to have been armed with
two MK 108 cannon. It was a high-wing monoplane
with almost square-planform wings with considerable
anhedral at the tips, and drawings showing two different
tail assemblies - one with a single dorsal fin and
high-set stubby tailplanes; the other with a single high
tailplane terminating in dorsal/ventral fins - were produced.
It is probably better considered as a manned
missile than an aircraft. There is no account of how
the pilot was supposed to complete the mission and
return safely to earth.
There is some question whether the 'Natter' actually
fits our criteria for Selbstopfermänner aircraft at
all, since the pilot was expected to break off his attack
and turn for home before ejecting (indeed, he was
provided with an escape system), but there is less
doubt in similar concepts put forward by Zeppelin
and DPS, both of which proposed what were essentially
motor-assisted gliders to be towed into attack
position by aircraft. The Zeppelin proposal - the
'Rammer' - had a solid-fuel rocket motor; the DPS
aircraft, which went into development as the Messerschmitt
Me 328, had an Argus pulse-jet like that
which powered the Fieseler Fi 103 flying bomb (qv).
There were high hopes of the latter, in particular, but
like the Ba 349, it never got past the prototype stage.
There was a third, very similar, project, the Sombold
So 334 'Rammschussjäger', which, despite its name,
was not actually intended to ram. It, too, was powered
by the Walter 509 motor and armed with rockets, and
ROCKET-POWERED AIRCRAFT
was to have been towed to operating height. Like the
Me 328, it started out as a parasite escort fighter project
but never got further than a wind tunnel model.
Blohm & Voss proposed a pure glider fighter, with no
powerplant at all, as the Bv 40. Armed with 30mm
cannon and towing a proximity-fuzed bomb on a
cable, the Bv 40 was to have been towed to a position
above the incoming bomber 'box' by a Bf 109 and
then released. Its limited acceptance was perhaps
indicative of the state of mind in Germany by 1944
when prototypes were built and tested.
THE ZEPPELIN'RAMMER'
The Zeppelin 'Rammer' never received an RLM designation,
which is an indication that perhaps it was
not taken entirely seriously. It was to have been a
small conventional aircraft with straight, constantchord
wings and tailplane, and was to have been
towed to its operational altitude by a Bf 109 or a Bf
110 and cast loose, whereupon it would start its
Schmidding 533 solid-fuel rocket motor and head for
the bomber formation, first firing its load of 14 R4M
5cm rockets and then trying to ram or sideswipe the
bomber aircraft, using its hugely strong wings. The
wing's leading edges were to have been covered in
3cm- (1.18in-) thick steel, and they were to have had
three continuous parallel main spars, fabricated from
thick-walled steel tubing, running from tip to tip to
slice through fuselage, tailplane or wings. The pilot,
who flew the aircraft in the prone position, was not
expected to take to his parachute, but was to have
landed the aircraft on any convenient piece of open
ground so that it could be recovered and re-used. It is
thought that no prototype nor even a mock-up of the
'Rammer' was actually constructed.
THE MESSERSCHMITT Me 328
The history of the Me 328 - which, like the 'Komet',
started life as a DPS project - began in 1941, rather
earlier than those of the other 'last-ditch' fighters. It
was concieved as an escort fighter, to be towed by a
Heinkel He 177 bomber on a semi-rigid bar (the
'Deichselschlepp' system, which was also under consideration
for use with manned glider bombers and
auxiliary fuel tanks) or mounted on a Dornier Do 217
or a Messerschmitt Me 264 in a 'Mistel'-like arrangement
(qv). A variety of versions were projected: a
pure glider; with Argus pulse-jets; and with a Jumo
004 turbojet. Only the pure glider and the pulse-jet
versions were produced (and then only in prototype
form). The ubiquitous Hanna Reitsch was responsible

ROCKET-POWERED AIRCRAFT

for completing a test programme on the two prototypes
of the glider version, cutting loose from tow
planes at altitudes of 3000-6000m (9800-19,700ft).
Ground launches, using both cable-type catapults and
rocket-assisted rail carriages, were also undertaken,
with equal success. Even with reduced wingspan, the
aircraft performed very satisfactorily, and it was
planned to build up to 1000 for use as disposable
bombers, to be flown by volunteers from 5/KG200,
the so-called 'Staffel Leonidas'.
Seven prototypes of the Argus pulse-jet-powered
version were built by a glider maker, Jacob Schweyer
Segelflugzeugbau. It was intended for use as a fighter
aircraft, to be armed with two MG 151 machine guns.
Tn static testing it soon became obvious that the same
problems which were to plague the early development
of the VI flying bomb - notably, excessive vibration
- would make the project difficult to bring to a successful
conclusion, and the manned flight programme
was suspended in mid-1944, after only a few test
flights had been made. Nonetheless, planning still
went ahead, and a version was projected, employing
no less than four Argus 109-014 pulse-jets, two
mounted below the mid-set wings in addition to the
original pair mounted above the rear fuselage, their jet
tubes protruding behind the fin below the tailplane.
Bomber versions of both these aircraft were also
proposed (and would actually have made greater
sense since the pulse-jet's characteristics were unsuited
to its use as a fighter powerplant). At Hitler's insistence,
work on the bomber version continued long
past the point when anything other than token use
Left: No more than 36 Ba 349s were constructed; none
was ever sent into combat, and most finished like these
three battered examples in the hands of GIs in Bavaria.
ROCKET-POWERED AIRCRAFT
Above: The Blohm & Voss Bv 40 was an unpowered glider
and was to have been towed into position above the
approaching bombers before making its attack.
could have been made of it. Perhaps the most farfetched
suggestion for a version of the Me 328 was
that with folding wings and twin pulse-jets, designed
to be launched from a catapult set up on the foredeck
of a submarine.
THE BLOHM & VOSS Bv 40
The simplest and cheapest - and perhaps the most
sensible - proposal for a Selbstopfermänner fighter
came from Blohm & Voss's Richard Vogt in mid-
1943. The Bv 40 was a simple small armoured glider,
armed with a pair of 30mm cannon and fitted with a
considerable degree of frontal protection, constructed
by unskilled workers from non-strategic materials,
which was to have been towed to a position above the
bomber formations by a Bf 109G and then cast loose
to prosecute a head-on diving attack. One proposed
innovation was the 'Gerät-Schlinge', which was really
nothing more than a towed aerial mine on a long
cable, and which was to be exploded when it was
within the bomber formation (although the bomb
tended to trail directly behind the glider, rather than
some way below it, and it was difficult to place as a
result). R4M rockets and 250kg (55()lb) bombs, to be
dropped into bomber formations from above, were
also suggested, as was a version to carry four aerial
torpedoes. Six prototypes were constructed, and five
flew before the project was cancelled in late 1944. In
an attempt to resurrect it, Vogt suggested fitting it with
Argus pulse-jets mounted under the wings, but he was
unsuccessful, the Me 328 having taken up what small
degree of enthusiasm existed for such a solution.

CHAPTER THREE
Hybrid Aircraft and
Gliders
During World War II, Germany made extensive use of unpowered aircraft in the
transport role, and though they met with diminishing success, they proved a useful
addition to the Reich's logistical fleet. In a parallel development, technology
developed for glider bombs was applied to the guidance of unmanned powered
aircraft too, the flight to the vicinity of the target being under the control of the pilot
of a single-engined fighter mounted piggyback on the explosives-packed bomber.
Even after the new German Air Force was established,
the unpowered aircraft still occupied an
important place in its order of battle, perhaps because
almost all Luftwaffe pilots recruited before Germany
openly re-armed had learned to fly in gliders. As we
have seen, many important new developments in aviation
sprang from the Deutsches Forschungsinstitut
für Segelflug (DFS).
Above: The DFS 230 carried Luftwaffe paratroops into
action against the Belgian fortress of Eben-Emael.
Left: The 'Mistel' was a fighter mated with an unmanned
bomber, the nose of which was an explosive charge.
THE DFS 230
Gliders were eventually to be developed in Germany
in all shapes and sizes and for a variety of roles. We
have seen them as both bombers and fighters, but they
were actually more effective, at least in combat terms,
as troop carriers and transports. The first to see action
was the diminutive DFS 230, a conventional glider
with straight, high aspect ratio wings, developed from
a prototype built by Rhön-Rossitten-Gesellschaft in
1932, which could carry eight combat-equipped soldiers.
In a very real sense, the DFS 230 was a secret
weapon par excellence, for in its combat debut, when
Luftwaffe paratroopers used it to assault and capture
the huge Belgian fortress at Eben-Emael on 10 May
45

HYBRID AIRCRAFT AND GLIDERS
1940, it achieved complete tactical and strategic surprise,
and allowed the Wehrmacht to cross into Belgium
virtually unopposed. Despite that success, once
their existence was known, gliders proved to be an
expensive way of getting infantry into combat, and
after a near disaster in Crete, were not employed in
that role by the Luftwaffe, although they were used in
an even more dramatic way in September 1943, when
commandos led by Otto Skorzeny landed 12 DPS
230s on a narrow strip of land in front of the Rifugio
Hotel on the Gran Sasso and liberated deposed Italian
dictator Benito Mussolini. From then on, it was left to
the Allies to employ them, notably in Sicily in July
1943, in Normandy in June 1944, and at Arnhem in
September of that year. That is not to say that the
Luftwaffe had given up on them by any means.
THE DPS 228 AND DPS 346
DPS later built a single prototype of a cargo-carrying
glider, the DPS 331, in 1941, but by that time the
main thrust of the Institute's work lay in the development
of high-performance experimental sailplanes.
The most significant of those was the DPS 228,
planned as a high-altitude photo-reconnaissance aircraft,
to be transported to an altitude of 10,000m
(32,8()()ft) or more and released, a rocket motor then
taking it to an altitude of 23,00()m (75,400ft). The
rocket motor was then to have been used intermittently
to maintain altitude until its fuel was exhausted,
whereupon the DPS 228 would glide back to friendly
territory. Depending on thermal conditions, it was
confidently expected that the aircraft would be able to
return from targets over 1000km (620 miles) away.
46
Above: The difficult and demanding Troika-Schlepp' -
requiring the service of three Bf 11 Os-was the original
method of getting a fully loaded 'Gigant' glider into the air.
Only a few were constructed. Many test flights were
made, all of them it is believed (though there are differing
reports) without rocket power, and a new pressurised
cabin, with the pilot in the prone position, was
eventually developed and tried out just days before
the war's end. Both the original cabin, in which the
pilot sat upright, and the later version, which was very
much more effective, were attached to the rest of the
airframe by explosive bolts. Set free, the nose cone
deployed a parachute and descended with the pilot
still on board until the outside temperature and pressure
reached life-supporting levels, whereupon his
seat or couch was ejected by compressed air and he
made a normal parachute descent.
A development of the DPS 228, the DPS 346, was
designed as a supersonic trials aircraft. It was to have
had two rocket motors, variable-chord swept wings
and a Multhopp-style T-tail, but was otherwise similar
to the DPS 228 in its later incarnation, although
constructed entirely of stressed aluminium rather than
wood. An unpowered prototype was to have been
built (in wood). It is believed that this aircraft and a
number of somewhat modified DPS 346s were constructed
in the Soviet Union after the war, and there
are persistent but unsubstantiated claims that the former
was the first aircraft to exceed the speed of sound
with DPS test pilot Wolfgang Ziese at the controls in
May 1947, some five months before Chuck Yeager's
supersonic flight in a Bell X-l on 14 October.

THE GIANT TRANSPORT GLIDERS
At the other end of the performance scale, two projects
to develop heavy-lift gliders capable of carrying
up to 22,000kg (48,5001b) of cargo - the approximate
weight of a combat infantry company, with all its
equipment - were ordered up by the RLM: one of
them from Messerschmitt, as the Me 321 'Gigant'
('Giant'); the other from Junkers, as the Ju 322
'Mammut' ('Mammoth'), originally named 'Goliath'.
The Messerschmitt aircraft was ultimately to be the
most successful by far, with about 200 built, but the
Junkers 'Mammut' was the more interesting of the
two, despite being a constructive failure.
THE Me 321'GIGANT'
The Me 321 was conventional in that it had a fuselage
to which the high-set wings and empennage were
attached. It was constructed from welded steel tubing
and wood with a covering of fabric and wood, and its
fuselage was rectangular in cross-section, very tall
towards the nose (which had clam-shell doors for
loading and unloading vehicles) and tapering towards
the tail, with side doors at the rear for passengers. The
cockpit was located on top of the fuselage, level with
the leading edge of the wing, which was straight and
tapered, with a span of 55m (180.5ft), braced by struts
to the fuselage floor at the point where the fixed
wheels were mounted. The tail was composed of a tall
fin and a braced tailplane. The aircraft performed perfectly
from the first flight, which took place at
Leipheim in March 1941, and was quite capable of
lifting the design payload. The first examples entered
service in May 1941, when a squadron of 18 was
formed. Originally, the 'Giants' were towed either by
a trio of Bf 110s (the so-called 'Troika-Schlepp') or
HYBRID AIRCRAFT AND GLIDERS
by a single Ju 290, and later by the specially developed
He l l 1Z 'Zwilling' ('Twin'), which was, in
effect, two He Ills joined at the wing, outboard of
the engines, the junction being effected at a fifth
engine, thus giving one outboard of each fuselage,
and three in the wing area between them. Rockets of
various types were mounted to assist take-off, and
there were plans to mount Argus pulse-jets to increase
the aircraft's gliding range after release. The principal
work of the 'Giant' was to transport material to the
Eastern Front. It had a crew of two and was armed
with four 7.92mm machine guns.
Even before the prototype glider had taken to the
air, work was in hand to transform it into a powered
aircraft. This consisted mainly of strengthening its
structure and contriving mountings for engines, initially
four supercharged Gnome-Rhone 14Ns, which
produced around 1150hp each. The prototype flew in
April 1942 and since it was considered to be underpowered,
the next aircraft had six engines, as did the
aircraft of all subsequent productions. The Me 323, as
it was designated, was something of a handful in the
air, requiring two flight engineers to keep the engines
balanced, and two gunners, with a total of five 7.92
mm (later 13mm) machine guns, plus locations for 10
MG34 infantry machine guns in the fuselage sides. It
often needed the assistance of a tow-plane or rocket
motors to get off the ground, especially when heavily
laden. It could carry around 16.25 tonnes (16 tons) of
payload, and had seats for 130 passengers (though
many more were carried in evacuation operations, for
Below: The heavily laden 'Gigant' - this is an Me 323 -
proved sickeningly vulnerable to air-to-air attack. In April
1943, no fewerthan 20 were shot down in one operation.
47

HYBRID AIRCRAFT AND GLIDERS
GOTHA Go 244B
Type: Transport
Length: 15.80m (51.83ft)
Span: 24.50m (80.38ft)
Above: Like the Messerschmitt 'Gigant', the much smaller
Gotha Go 242 also made the transition from glider to
powered aircraft, becoming the Go 244 in the process.
example). It first became operational in November
1942, and was used to supply units of the Afrika
Korps from a base in Sicily. Although it was largely
successful, it did have its spectacular failures. On 22
April 1943, no less than 21 Me 323s, ferrying petrol,
were shot down in a single operation. Production
continued until m id-1944, and around 200 examples
were built in all.
THE Ju 322'MAMMUT'
The heavy glider Junkers produced was anything but
conventional. Designed by Heinrich Hertel, it was
simply an enormous flying wing, inside which it carried
almost all of its payload, with a tall fin carried on
a boom-like extension at the tail. In overall form it
was somewhat reminiscent of the Junkers-G 38, a
commercial passenger-carrier which made its first
flight in 1929. On RLM instructions, the Ju 322 was
constructed entirely from wood. With a span of 62m
(203.5ft) and a length of 30.25m (99.25ft) it had a
wing area of 925m 2 (9952 sq ft). The centre section of
the wing's straight leading edge housed a top-hinged
loading door, with a glazed cupola to the port side of
it containing the flight deck. The upper surface of the
wing was flat, and there was considerable dihedral on
the lower surface. At the centre point, it was over 3m
(9.8ft) thick. The prototype did fly in April 1941 but
by that time its payload had been cut to half of the
required 22.35 tonnes (22 tons) as the 'cabin 1 floor
was simply not up to the task: a tracked vehicle actually
broke through it during loading trials and the air-
48
Max take-off weight: 7800kg (17,196lb)
Max speed: 290km/h (180mph) at 3000m (9800ft)
Range: 740km (460 miles}
Armament: 4 x 7.92mm MG 34 machine guns
craft proved to be chronically unstable. It landed safely
and was towed back to the airfield at Merseburg.
Given a larger tail fin in an attempt to counter the
instability, it made a few more test flights before the
project was abandoned on the orders of the RLM. It
was then cut up for fuel, along with a completed second
aircraft and the components of 98 more which
were already in the process of construction.
THE GOTHA Go 242/244
Somewhat more practical than either of the giant gliders
and more numerous by far was the Gotha Go 242.
It was a shoulder-wing monoplane with a simple
square-section fuselage culminating in twin booms
linked by a cross-plane to form the tail. A loading
ramp at the rear of the fuselage pod let down to allow
loading and unloading of a small vehicle such as the
amphibious Kübelwagen, or 21 fully equipped troops.
Over 1500 were built, of which 133 were converted
into Go 244s, fitted with two VOOhp Gnome-Rhone
engines in forward extensions of the tailbooms.
A few of the gliders were converted to allow them
to alight on water; they carried a small catamaran
assault boat with a 1200kg (26461b) explosive charge
suspended between its hulls. The mission profile
envisaged for them saw the pilot setting down near an
enemy ship and taking to the assault boat, setting off
in it at high speed toward the ship and locking the
controls before baling out to be rescued later by seaplane
or submarine. No such mission ever took place,
though it is worth remembering that members of the
Italian Navy's Xth MAS flotilla disabled the cruiser
HMS York with explosive-packed motor boats at Suda
Bay in Crete in March 1941, so the idea was not that
far-fetched.

HYBRID AND COMPOSITE AIRCRAFT
Engineers on both sides during World War II gave
considerable thought to the problems associated with
guiding unmanned explosives-packed aircraft to a target.
We shall see in Chapter Five how the USAAF
used remotely controlled B-17s to complete the
destruction of V weapons sites in France in 1944, but
long before that, in 1940, the RLM had turned the
problem over to DPS. The parameters the Institute
was given included supporting parasite fighter aircraft
and refuelling heavily loaded bombers in flight as
well as guiding a flying bomb to its target zone, and
the first tentative solution was to tow one aircraft with
another using either a flexible cable or a semi-rigid
bar which could contain or support a fuel hose. There
was a persistent belief that such a system had merit,
and experiments with it continued until 1945, but by
late 1941, one of the Institute's teams had begun to
work on a means of mounting one aircraft on another,
piggyback-style, and in January 1942 the 'Mistel'
('Mistletoe') concept received official approval.
Soon, Junkers and autopilot-maker Patin were
ordered to collaborate with DPS, and within little over
a year, work had begun on assembling a prototype
combination of Ju 88A-4 and Bf 109F-1.
'MISTEL' 1
DFS's first task had been to devise a suitable structure
to co-locate the two aircraft so that the stresses acting
on them would be transmitted between the two main
spars, with coupling links which could be sundered
either mechanically or explosively. The result was a
pair of tripod struts, the apex of which hooked into
plates on the underside of the Bf 109's wing roots, the
HYBRID AIRCRAFT AND GLIDERS
two outer bases of each located on load-bearing plates
which traversed the main spar, while the inner legs
located on to it directly through the fuselage top. A
single pole supported the Messerschmitt's tail and
kept the fuselage axes parallel. In later combinations,
the fighter sat at a 15-degree nose-down angle.
The steering and control system was located in the
rear of the Junker's fuselage and consisted of a master
compass, a steering compass and a three-axis
autopilot from Patin. This apparatus was used to steer
the combination in normal flight via servos and two
simple thumb switches in the fighter's cockpit, one
for rudder and ailerons, the other for elevators, with
the fighter's controls remaining free. However, the
two aircraft's control systems could be linked, and
thus operated from the fighter by the usual combination
of stick and pedals (via servos, once again), at
will. Either the bomber's two engines alone, or all
three, could be used, depending on the speed and
range required, all fuel being supplied from the host
aircraft. This was by no means the only modification
needed to the bomber component - in fact, the aircraft
were virtually gutted and rebuilt - but the amount of
work needed on the fighter was minimal. In order to
accommodate the explosive 'warhead', the existing Ju
88 nose section, including the glazed cupola which
formed the cockpit cover, was removed entirely, and a
solid bulkhead built up. The 3500kg (7720lb) hollow
charge, with its distinctive proboscis-like extension
Below: One of the earliest'Mistel' combinations (they
were known unofficially as 'Vater und Sohn' - father and
son) matched the Messerschmitt Bf 109F with the Junkers
Ju 88A-4. Testing began in July 1943.

HYBRID AIRCRAFT AND GLIDERS
'MISTEL' 1
Combination: Ju 88A-4 plus Bf 109F-4
Powerplant (Ju 88): 2x Junkers Jumo 211J
Powerplant (Bf 109): 1 x Daimler-Benz 601N
Payload: 3500kg (7720lb) hollow charge;
1000kg (2200lb) steel core
Above: The operational 'Mistel' (this page) paired a fighter
with a bomber whose nose was replaced with a warhead.
Trainers (facing page) retained the standard nose.
and 1000kg (22001b) steel core, could then be mounted
on the bulkhead; for training missions, a standard
two-man nose section, stripped of all non-essentials,
could be mounted in its place. Operationally, the procedure
of launching the bomber component was
straightforward. The pilot lined the combination up
with the target in a shallow dive using his standard
reflecting gunsight, activated the automatic pilot, and
then broke free. Some elected to attempt to suppress
local flak before setting out to return to their base.
'MISTEL TARGETS REVEALED
The first flight of the combination took place in July
1943, and the testing procedure was successfully
completed by October, by which time development
work on the warhead was well advanced and 15 combinations
had been ordered from Junkers, who were
responsible for the conversion itself. By April 1944, a
small unit, designated 2/KG101, and under the command
of Hauptmann Horst Rudat, had been set up and
had begun training, initially at the Junkers airfield at
Norhausen, later at Kolberg on the Baltic coast. In
mid-month, a staff paper outlined the targets for the
unit (initially with just five pilots) as shipping in
Scapa Flow, Gibraltar Roads and Leningrad, though
the latter two were soon rejected as being impractically
far away. Scapa Flow was chosen as the first
objective, and the aircraft were to take off from Grove
in Denmark and cross the North Sea following a line
of pre-positioned radio buoys. Planning had reached a
fairly advanced stage when the Allies landed in Normandy,
and in mid-June, 2/KG101 moved to St
Dizier, from where five 'Mistels' took off just after
dark on 24 June to attack shipping in the Baie de la

Seine. Four of the five aircraft involved were reported
to have hit shipping targets, the fifth pilot jettisoning
his host bomber after a mechanical failure.
Over the course of the next four months, more
units were trained in the operation of the combination
and two more 'Mistel' raids took place, one on shipping
in the English Channel, the other on Scapa Flow.
Neither was successful. In the course of the latter,
three aircraft crashed and the other two failed to find
the target. By now, other combinations had been
ordered which paired more recent models of the Ju 88
with Fw 190s, and the factory at Bernberg was producing
them from new - not re-cycled - aircraft.
Attention turned east in November 1944, and training
for Operation 'Eisenhammer' commenced, which was
a campaign aimed at destroying electrical power stations
in the Soviet Union. As the Allied armies closed
in on the Reich from east and west, bridges in particular
became important targets, and through the spring
HYBRID AIRCRAFT AND GLIDERS
'MISTEL'SI
Combination: Junkers Ju 88A-4 plus
Messerschmitt Bf 1Ü9F-4
'MISTEL' S2
Combination: Junkers Ju 88G-1 plus
Focke-Wulf Fw190A-8
'MISTEL S3c
Combination: Junkers
Ju 88G-10 plus Focke-
Wulf Fw190A-8
of 1945, it was against river crossings and bridgeheads
that the 'Misteln' were used exclusively. The
last operation took place on 16 April 1945.
Many other combinations of aircraft types were
projected (and in some cases built) for use in 'Mistel'
operations, including Dornier Do 217K/DFS 228, for
reconnaissance, the host aircraft acting as a mobile,
high-altitude launch pad; Do 217/Fw 190, for
pathfinder missions, the fighter protecting the host
aircraft; and Ta 154/Fw 190, Me 262/Me 262, Ju
287/Me 262 and Ju 268/He 162 combinations, all of
which were proposed for use against high-value targets,
where approach speed might have been thought
to make ä significant difference. By 1945, DFS was
working on remote-control systems using both the
radio link and the television guidance system specially
devised for the Hs 293 guided bomb (see Chapter
Seven). A test aircraft had been prepared, but it was
destroyed by fire before trials could begin.

CHAPTER FOUR
Rotary-win g
Aircraft
Rotary-wing aircraft were first demonstrated as early as 1907, but it was 1936 before
a satisfactory design for a helicopter was developed, in Germany. The Reich's
scientists took the lead in this field, and by 1945 had developed operational rotarywing
craft and demonstrated just how effective they could be in combat conditions.
Rotary-wing aircraft can be divided into two basic
types: autogiros and helicopters. Autogiros, such
as that devised by Juan de la Cierva, derive their lift
from their forward momentum, which is supplied by
a conventionally positioned propeller, and their rotors
are unpowered. They can take off only with a run,
they cannot fly except in the forwards direction, and
Above: The Flettner Fl 282 'Kolibri' was a fully operational
helicopter despite its somewhat rudimentary appearance.
Left: 'Dare anything' test pilot Hanna Reitsch shows off
the Focke Achgelis Fa 61 inside Berlin's Deutschlandhalle.
they cannot hover, but they can descend and land
almost vertically. Cierva made the first successful
flight in an autogiro in January 1923, having found
that it was necessary to articulate the blades where
they joined the hub. For some years, autogiros seemed
set to overshadow true helicopters, examples of which
had been flying since 1907, but once Cierva's articulated
rotor head arrangement was adopted, the latter
surged to the fore once more, although work on autogiros
continued, too. By the late 1930s, Germany had
become the centre of helicopter development; in the
period up to May 1945, almost 20 rotary-wings of different
types were designed there, including autogiros,

girogliders and manned kites. The only work of any
note undertaken elsewhere was that of the Russian
emigre Igor Sikorsky in the United States. Sikorsky
made his first experiments with rotary-wing flight in
1909, but did not achieve comparative success until
30 years later, though he was to become crucial to the
type's development.
THEFOCKEACHGELISFaGI
In the early 1930s, Professor Heinrich Karl Focke
began building CiervaC.19 autogiros under licence in
Germany - and separately from his partnership with
Georg Wulf - and soon began experimenting with
helicopters. Focke collaborated with Gerd Achgelis,
who flew a Kurt Tank-designed Fw 44 'Steiglitz'
('Goldfinch') in aerobatics displays (as did Ernst
Udet), and soon produced a design for a twin-rotor
helicopter, the Fa 61. This resembled the Cierva
machine in that it was composed of a conventional
fuselage with a front-mounted radial engine (a BMW
Bramo Sh 14, of 160hp), but differed in having two
outrigger-mounted three-bladed rotors, driven by
shafts in centra-rotation to neutralise torque effect.
There was a small conventionally placed propeller,
but only to assist engine cooling. The tail had a fin
and rudder and top-mounted stabilisers, and the craft
sat on a tail-wheel undercarriage but with a nose
wheel to prevent it from nosing over. The rotors had
cyclic pitch control (that is, the angle of attack of the
individual blades was varied during the rotation
cycle) which gave longitudinal and directional control,
and differential operation of the two cyclics gave
Above: The Fa 223 'Drache' {'Kite') was the first truly
viable transport helicopter. This example was constructed
in Czechoslovakia after the war, from salvaged parts.
lateral control by inducing asymmetric lift. The Fa 61
made its maiden flight in the hands of Ewald Rohlfs
on 26 June 1936, lasting 28 seconds. But by the following
year, Rohlfs was setting and breaking records
regularly. On the anniversary of the maiden flight, he
established a height record of 2440m (8000ft) and an
endurance record of lhr:20min:49sec. The following
day he set straight-line and curcuit distance records
and a speed record of 122.553km/h (76.1 mph) over a
20km (12.5 mile) course. Hanna Reitsch broke the
straight-line record with a flight of almost 109km
(67.7 miles) between Bremen and Berlin four months
later, and in February the following year, she actually
flew the helicopter inside the Deutschlandhalle in
Berlin to demonstrate its controllability. On 29
January 1929, Karl Bode established a height record
which was to remain unbroken for some time when he
took the machine to 3427m (11,240.5ft).
The Fa 61 was hardly a secret weapon. Indeed, it
was developed very publicly and was really little
more than a concept demonstrator, but there was
much better to come both from Focke Achgelis and
from a competitor, Anton Flettner, during the course
of the war. The Wehrmacht was quick to appreciate
the operational possibilities the type opened up. In
1938 Focke Achgelis began work on a genuine transport
helicopter known originally as the Fa 266
'Hornisse' ('Hornet'), and later as the Fa 223

'Drache' ('Kite'). The new aircraft was essentially an
enlarged version of the Fa 61, with the same boomedout
twin-rotor layout, but it was much more powerful,
with a supercharged 650hp Bramo 323 Q3 'Fafnir'
engine, and more flexible and easier to fly, thanks to
the introduction of collective pitch control.
Previously, ascent had been controlled by the throttle,
a very hit-and-miss affair; with the introduction of
collective pitch control, the degree of lift was controlled
by adjusting the pitch of the rotor blades, and
engine speed stayed constant. The fuselage, 12.25m
(40ft) long, was fabricated from steel tubes and covered
with fabric except on the engine compartment,
where sheet metal was used. It was divided into four
compartments: the cockpit, with seats for pilot and
observer; the load compartment, with a starboard-side
door, where self-sealing fuel and oil tanks were also
located; the engine compartment; and the tail section,
which was a conventional fin and rudder with a topmounted
stabiliser, adjustable for trim.
UNUSUAL ENGINE MOUNTING
The method of mounting the engine was somewhat
bizarre. Both it and the gearbox were located in two
large-diameter rings, which were attached to four longitudinal
fuselage members by adjustable cables, with
struts to prevent fore-and-aft movement. There was a
gap in the fuselage covering at the forward end of the
engine compartment, through which cooling air
entered, and another at its after end, whence it
escaped. The rotor blades were made from wooden
ribs attached to a high-tensile steel tube, and covered
with plywood and fabric. The rotor discs were
inclined inwards by 4.5 degrees, and slightly forwards,
and normal speed of rotation was 275rpm, a
9.1:1 reduction from engine speed.
The 'Drache' (it was also known as the 'Draken':
'Dragon') could carry up to four passengers in the
load compartment but during troop manoeuvres in
1944, it carried 12 fully equipped soldiers, the other
eight travelling outside on tractor seats on the outriggers.
Its total payload capacity was around 1.27
tonnes (1.25 tons). A Fieseier 'Storch' aircraft and a
Volkswagen car were lifted in demonstrations, and
small field pieces were transported during army
manoeuvres; large loads were slung from a winch on
a load-bearing beam via a port in the aircraft's floor.
The Fa 266 prototype was completed at the end of
1939 and, by now redesignated as the Fa 223, made
its first free flight in August 1940 after more than 100
hours of static and tethered hovering trials. Karl Bode
ROTARY-WING AIRCRAFT
flew it to the RLM test centre at Rechlin in October
1940, and set a batch of new records: a speed of
182km/h (113mph); a vertical rate of climb of 528m
(1732ft) per minute; and an altitude of 7252m
(23,295ft) where normal operational limits were
120km/h (74.5mph) and 4880m (16,010ft). The RLM
promptly ordered 30 for evaluation in the anti-submarine,
reconnaissance, rescue, training, and transport
roles and it was decided before series production
commenced to build standardised aircraft which
would be equipped according to the requirements of
their mission.
The first prototype, -VI, was wrecked on 5
February 1941 after having made 115 flights, when a
power failure occurred while it was in a low hover. In
June 1942, the second and third prototypes, along
with seven pre-production machines and much of the
tooling, were destroyed in an air raid. Production was
then moved from Bremen to Laupheim in southern
Germany but did not restart until February 1943.
More aircraft were destroyed when the new factory
was bombed in its turn, in July 1944, and as a result,
the number of Fa 223s completed was probably no
more than 12. Three were still in operational service
at the end of the war; one was destroyed by its pilot
and two were seized by the Americans. One of them
was subsequently flown to England by Helmut
Gersenhauer, the Luftwaffe's most experienced helicopter
pilot, and was flown for around 170 hours in
trials before crashing from a height of 18.3m (60ft).
After the war, development of the Fa 223 continued in
France (with Professor Focke's assistance) and in
Czechoslovakia, where two were constructed from
salvaged parts. That the Fa 223 was not more widely
produced, when all concerned agreed that it was a
useful addition to the Luftwaffe's catalogue of aircraft,
is understandable only within the terms of the
struggle for the allocation of resources going on within
the Third Reich at the time. Clearly, it had no
champion sufficiently powerful to push it high
enough up the list of priorities. Had -V12 not broken
down when transporting the captured Italian dictator,
Benito Mussolini, from the hotel on the Gran Sasso in
September 1943 when he was rescued by Otto
Skorzeny, perhaps things might have been different!
THE Fa 225
The Luftwaffe's interest in gliders dated back to the
time before Germany was permitted an air force,
when the only means she had of training pilots was to
set up gliding clubs and schools. As well as acting as

ROTARY-WING AIRCRAFT
Above: The Fa 330 was not a true helicopter but an
unpowered girokite; it was designed to be towed behind
a submarine as an observation platform.
a valuable means of instructing personnel, gliders
were to become important in themselves in a number
of roles. The first operational use of a glider to transport
troops and equipment directly into combat
occurred on 10 May 1940, when Luftwaffe paratroops
siezed and held the Belgian frontier fortress of
Eben-Emael after landing on it in DPS 230 gliders.
This was to be the most effective type in German service
during World War II, but it could be employed
only where there was a suitable, fairly large, landing
site. Focke Achgelis suggested improving on this by
substituting a three-bladed rotor unit from an Fa 223
for the wings of a DFS 230, producing what was in
effect an externally powered autogiro or giroglider,
which, when cast loose, would simply autorotate to
the ground at a very steep angle of approach, and
would thus be able to land in an area not much larger
than itself. It was to be towed behind the Luftwaffe's
maid-of-all-work, the Ju 52, and in tests carried out
during 1943, it was found to be practicable to land it
and come to a halt within 18.3m (60ft). Though the
Fa 225, as the hybrid glider was known, worked well
enough, by the time it was ready to go into production,
the Wehrmacht's operational requirements had
changed and the project was shelved.
^R
THE Fa 330'BACHSTELZE'
The Fa 225 was not the only unpowered rotary-wing
aircraft Focke Achgelis was to design. Early in 1942,
the company was asked to devise a simple single-seat
girokite to be towed behind a submarine, from which
an observer would be able to monitor a much wider
area than would a look-out stationed on the boat
itself. The result, the Fa 330 'Bachstelze' ('Water
Wagtail'), was simple in the extreme: two steel tubes,
the shorter, which supported the rotor assembly,
being set at right-angles to the longer, which held the
simple rudder assembly and the pilot's seat and rudimentary
controls, by means of which he could tilt the
rotor head (which gave longitudinal and lateral control)
and turn the rudder to change direction. The
pitch of the rotor blades could be adjusted, but not in
flight. Coarse pitch gave the best flying performance,
but made launching rather more difficult. The Fa 330
was launched by setting the rotor turning (by hand if
there was a wind; by means of a rope wound around
a drum in the rotor head if there was not) and then
pushing the whole machine backwards. Recovery
was by means of a winch under normal circumstances,
but in an emergency, the pilot could release
the rotor, which deployed a parachute from its
stowage behind the pilot's seat as it flew off. The
winch held 150m (492ft) of towing cable, which permitted
the kite to fly at an altitude of 120m (395ft);
from there, the horizon was 4()km (25 miles) away, a
marked improvement over the 8km (5 miles) horizon
from the boat itself. Without its pilot, the girokite
weighed 82kg (1801b), and could be assembled and
dismantled in a matter of minutes. Minimum speed
required to stay aloft was 27km/h (17mph).
Something like 200 Fa 330s were produced by
Weser-Flugzeugbau and were deployed aboard Type
IX ocean-going U-boats, but little is known about
their operational history beyond the fact that two or
three crewmembers from each boat were taught how
to fly them in the wind tunnel at Chalais-Meudon
near Paris. They were said to be very easy indeed to
operate, and would fly quite happily hands-off for
short periods, but were unpopular with their pilots for
reasons of self-preservation.
AMBITIOUS FOCKE DESIGNS
Focke Achgelis also produced two very much more
ambitious designs, one of them, the Fa 269, for a convertiplane,
which would have landed and taken off
vertically but then turned the shaft carrying the rotors

through 90 degrees to bring them to the position of
pusher propellers. Such an arrangement (but employing
more efficient tractor propellers) was not to be
successfully introduced until Boeing-Vertol perfected
the V-22 Osprey in the late 1980s. The Fa 269 was
really little more than a flight of fancy, and it is to be
doubted if the technology of the day could actually
have realised it. The Fa 284 was much more practical,
being, in effect, a stretched version of the Fa 223, with
a fuselage which was largely of lattice construction
and twin 1600hp BMW 801 engines. Tt was designed
to carry heavy loads underslung, in exactly the same
way as its 1970s equivalent, the Sikorsky S-60 (CH-
54B) 'Flying Crane', did. Some parts are said to have
been manufactured before the project was cancelled
in late 1943 and plans were drawn up to produce a
twin Fa 223, essentially two aircraft joined, in-line, by
a short fuselage section. This section is known to have
been produced, but the complete aircraft was not.
By far the most adventurous of Professor Focke's
designs was presented under the auspices of Focke-
Wulf rather than Focke Achgelis. Known as the
'Triebflügel' ('Thrustwing'), this was a tail-sitting
VTOL (Vertical Take-Off and Landing) aircraft which
derived its lift from three wings which rotated around
the fuselage just aft of the cockpit, under the power of
tip-mounted ramjets giving about 840kg (18501b) of
thrust, the wings being brought up to operating speed
by three jettisonable rockets. In flight, the wings
would be rotated around their individual axes until
ROTARY-WING AIRCRAFT
they became conventional aerofoils as the aircraft
itself rotated until its axis was horizontal rather than
vertical. No real development work was ever done on
the concept, and the viability of the design is a matter
of speculation, but three tail-sitting VTOL aircraft
were built post-war, two in the USA and one in
France. The American designs, from Lockheed and
Convair, were somewhat more conventional, in that
they used fixed wings and contra-rotating propellers
in the nose, while the French SNECMA 'Coleopter'
was powered by a tail-mounted turbojet and had an
annular wing, control being achieved through four
swivelling fins. All three aircraft flew after a fashion,
but all projects were eventually cancelled. The objective
has since been achieved by vectoring the thrust of
a turbojet in a more-or-less conventional airframe.
ANTON FLETTNER
Having turned his attention to the problems of rotarywing
flight in 1930, Anton Flettner first produced a
helicopter with two 30hp Anzani piston engines
mounted on the ends of two rotors, each turning a
two-bladed propeller. While this arrangement eliminated
the problems associated with torque (which the
Focke Achgelis designs overcame by means of two
contrarotating rotor sets, and which other designers,
Below: The Fl 282 was the most sophisticated of all
German helicopters of World War II. This later version -
captured by US forces - even had protection for the pilot.

ROTARY-WING AIRCRAFT
notably Sikorsky, counteracted by means of a powered
tail rotor), it was only marginally successful in
other ways. When it was destroyed during tethered
testing, it was not rebuilt. Flettner next built a twoseat
cabin autogiro for the Kriegsmarine (German
Navy) but the single example of the Fl 184 caught fire
in flight and was also destroyed.
THE Fl 185 AND Fl 265
Clearly, Anton Flettner was still searching for a valid
way forward, for his next design, designated the Fl
185, was substantially different again, almost a cross
between a helicopter and an autogiro, its 140hp
Siemens-Halke engine being linked to a single rotor
and two variable-pitch pusher propellers located on
outriggers. For vertical take-off and landing, the aircraft
functioned as a helicopter, the majority of the
power going to the rotor, and the two conventional
propellers, providing thrust in opposite directions,
only counteracting the torque. For forward flight, the
rotor autorotated and the two propellers received all
the power and gave forward thrust. The Fl 185 flew
only a few times before Flettner abandoned it and
turned his attention to a new design using synchronised
intermeshing contra-rotating twin rotors (like
those of the Kaman H-43 'Huskie' of the 1960s) with
differential collective pitch control.
The single-seat Fl 265 was very similar in appearance
to the Fl 185, with its front-mounted radial
engine with cowl and cooling fan, enclosed cockpit
Below: The Fl 282 was ordered in 1944 after sea trials
aboard the cruiser Köln had shown it could be flown even
in adverse conditions. Only Allied bombing prevented the
aircraft going into service.
R8
FLETTNER Fl 282 V21
Type: Single-seat opencockpit
helicopter
Length: 6.56m (21.52ft)
Max take-off weight:
1000kg (2200lb)
Max speed: 150km/h
(93mph) at sea level
Range: 170km (106 miies)
Ceiling: 3290m (10,800ft)
Armament: None
and stubby tailfin. However, gone were the Fl 185's
outriggers and propellers, and the rotor head assembly,
with its paired, inclined shafts, each with a twobladed
rotor, was much more complex. The design
was completed in 1937, and the following year, the
Kriegsmarine ordered six aircraft for evaluation purposes.
The prototype made its maiden flight in May
1939, and was later destroyed when its rotor blades
struck each other in flight.
Other Fl 265s were used extensively for operational
trials with naval units - cruisers in the main, but
also submarines - in the Baltic and the Mediterranean
with considerable success, and completely validated
the concept of deploying VTOL aircraft with warships.
Aircraft also operated with army units, both in
the reconnaissance and logistical roles, and a
Luftwaffe trial involving a Bf 109 and an Fw 190 fitted
with camera guns demonstrated that the helicopter
was very difficult to shoot down. The two fighters,
amongst the best in the world, we may recall, attacked
the Fl 265 for 20 minutes but tailed to score a single
hit. The outcome of the various trials was that Flettner
was ordered to proceed with volume production. In
fact, he had already proceeded with the design of an
updated version, the two-seat (some prototypes were
single-seat) Fl 282 'Kolibri' ('Hummingbird'), and it
was this aircraft which went into manufacture.
THE Fl 282'KOLIBRI'
The most important modification Flettner made to the
design of the new aircraft was to re-locate the engine
behind the pilot's seat, which gave him and the
observer a much-enlarged field of view. The drive was
taken off the front of the crankshaft through a reduction
gearbox and transmitted up and back through a

universally jointed drive shaft and a cross-shaft connecting
the two rotor shafts, which were set at an
inclusive angle of 24 degrees, and inclined forward
by 6 degrees. The rotor blades were mounted so that
they were parallel when they were at 45 degrees to
the aircraft's centreline. The fin and rudder were
much larger than in previous Flettner designs, steering
being accomplished by a combination of rudder
movement and differential collective pitch control.
The 'Kolibri' proved to be very satisfactory
indeed, despite a pronounced vibration period as the
engine was run-up, with a maximum speed in level
flight of 150km/h (93mph), a vertical rate of climb of
91.5m/min (300ft/min), a hover ceiling of 300m
(985ft), and a service ceiling of 3290m (10,800ft). Its
range, with just the pilot and maximum fuel aboard,
was 300km (185 miles). Some 50 pilots were trained
to fly it, most of them by Flettner's test pilot, Hans
Fuisting. It was extremely manoeuvrable and very
stable and at forward speeds in excess of 60km/h
(37mph) could be flown hands-off once the controls
were balanced.
SEA TRIALS
From 1942, trials at sea aboard the cruiser Köln
demonstrated that the aircraft was usable even in very
poor weather conditions, and by the following year,
20 were in service with the Kriegsmarine in the
Mediterranean and the Aegean. In 1944, an order for
1000 Fl 282s was placed with BMW, which began
tooling up for production at its Munich and Eisenach
plants, but before manufacture could begin, both they
ROTARY-WING AIRCRAFT
Above: An American airman examines the tiny rotor-tip
jets which Friedrich von Doblhoff proposed to use to
eliminate the effects of engine torque in his WNF 342.
and the Flettner works at Johannisthal were very
badly damaged by Allied bombing. Anton Flettner
went on to design a 20-seat passenger helicopter, the
Fl 339, but never got beyond the development stage.
THEDOBLHOFF/WNF342
Friedrich von Doblhoff is rather less well-known than
the other helicopter pioneers in the Third Reich, but
the machines which he designed, and which were
built by Wiener Neustadter Flugzeugwerke in the
Vienna suburbs, represented yet another innovatory
approach to the solution of the torque problem.
Doblhoff used small rotor-tip jets to drive the blades.
A combustible air/fuel mixture was fed to small combustion
chambers in the rotor tips using a compressor
driven by a conventional piston engine. The mixture
travelled by way of the rotor hub and passages in the
rotors themselves, before being ignited. The piston
engine also drove a small fan which blew air over the
tail surfaces for the purpose of steering. Only four
prototypes were built; the first three had fixed-pitch
blades, and were only ever used in static/tethered
tests, but the fourth had a most ingenious (and very
complex) arrangement which allowed collective pitch
control. The last prototype was behaving well in its
trials and had been flown at speeds of up to 45km/h
(28mph) when the programme was halted by the
arrival of Soviet forces in 1945.

CHAPTER FIVE
Surface-to-Surface
Missiles
Until the outbreak of World War II, rocketry was hardly a science at all; until then it
had consisted of really nothing more than a few scattered and sporadic attempts to
shoot small projectiles straight up into the sky, virtually for the sake of it. All that
changed when it became clear that the rocket had potential as a long-range weapon
of war, and nowhere was this potential better understood than in Germany, where
much of the pioneering work on rockets had been done anyway.
Most famous of the German secret weapons of
World War II - and by far the most effective -
were the surface-to-surface missiles used to bombard
the United Kingdom and targets on the mainland of
Europe, particularly the port of Antwerp, from late
June 1944. As well as the so-called 'Vengeance
Weapons', the VI and V2, there were other types
(though only one was operational, and then only in a
Above: The Fi 103 R-the manned VI.
Left: This A4 - or V2 - was captured by British forces and
fired by British scientists near Cuxhaven in 1945.
very limited sense), designed to supply data on flight
characteristics and to act as concept vehicles for operational
types. Not surprisingly, given the success of
the V2 ballistic missile, there were plans to develop it
still further, though none passed the prototype stage,
and most existed only on paper. Many of the scientists
and engineers who worked on Germany's rocketry
programme went on after the war to become prime
movers in the rocketry and space exploration programmes
of both the United States of America and the
Soviet Union, and were thus instrumental in both
putting man into space and establishing a technology
which has become a mainstay of modern civilisation.

SURFACE-TO-SURFACE MISSILES
THEFIESELERFM03-THEV1
The Vergeltungswaffe l (the revenge, or retaliation,
weapon), or V1, had a plethora of names. To the Luftwaffe,
it was the Fliegerabwehrkanonezielgerät 76
(Flakzielgerät 76, or just FZG 76), but that was a
cover-name: Fliegerabwehrkanonezielgerät means
'anti-aircraft gun aiming device' or conceivably 'antiaircraft
gun target device'. Its official codename was
'Kirschkern' ('Cherrystone') and it was also known as
'Krahe' ('Crow'); while to the RLM it was the Fi 103;
and to the airframe manufacturers, Fieseler, it began
life as P. 35. To the British public it was the Buzzbomb,
the P-Plane or the Doodlebug, while the RAF
knew it as 'Diver'. In effect a first-generation cruise
missile, it was an unmanned air-breathing jet aircraft
with an explosive warhead and a simple guidance/targeting
device, and to relate its history from the very
start, we need to go back to 1928.
Paul Schmidt worked primarily in the associated
fields of fluid dynamics and aerodynamics, but in
1928 he began experimenting with a simple form of
thrust engine known as a pulse-jet. In essence, a
pulse-jet is a tubular combustion chamber with a
matrix of small, rectangular, spring-loaded flapvalves
at the front, into which a suitable fuel (it need
be no more exotic than petrol, and low-octane petrol,
at that) is injected. The device must be accelerated by
Above: The infamous V1 self-propelled guided bomb. The
proto-cruise missile carried a warhead of 830kg (1832lb)
of amatol to targets up to about 240km (150 miles) away.
Below: The Argus pulse-jet - small flaps in the aperture
were forced open against a spring by air pressure and
forced shut by fuel exploding in the jet pipe behind.

some external means to a critical threshold velocity,
something of the order of 300km/h (I86mph), before
it will work, though there is the option to supply it
with air under sufficient pressure and in sufficient
quantity by means of a blower system. As the device
travels forward, air is forced past the flap-valves and
into the tube; the act of opening the flap-valves opens
a second valve, which admits a quantity of petrol
under pressure into the tube to form an explosive mixture
(in exactly the same way that a petrol engine's
fuel injection system does), and also activates a sparking
plug. The primary result of the explosion is to
blow shut the flap-valves, closing off both air flow
and petrol flow, and this has the secondary effect of
turning aimless explosion into directed thrust. As the
pressure within the tube is reduced to below that of
the air trying to rush into the engine from the front,
the flap-valves are forced open again, and the whole
process is repeated, and so on, many times per second;
for example, the Argus 109-014 engine used in
the operational Vis cycled 47 times per second.
CHEAP AND SIMPLE
In addition to its inability to self-start, the pulse-jet
motor has other limiting factors: it works less effectively
as the ambient air pressure drops, and functions
poorly at much above 3000m (9800 feet); it operates
at a fixed speed, though the dimensions of the combustion
chamber can be varied to modify it; and the
flap-valves are liable to burn out after a relatively
short time. But it has several things in its favour, too:
firstly, it works; secondly, it is simple to manufacture;
and thirdly, it costs very little.
All in all, it was just the thing to power a shortrange
surface-to-surface missile, and this was one of
the uses Schmidt suggested for it after failing to interest
anyone in a vertical take-off aircraft powered by it.
He submitted a design to the RLM in 1934. Initially it
was poorly received, but after a number of rather
more eminent scientists, including Wernher von
Braun, took up Schmidt's case, both the RLM and the
Heereswaffenamt (HWA - the German Army's
weapons development and procurement office) took
more notice. At last Schmidt got development funds,
even if not in great amounts. By 1940, Schmidt's
pulse-jets were giving over 500kg (1 lOOIb) of static
thrust, but the RLM had started to look elsewhere for
alternative developers. It looked, in fact, to the rather
more prestigious Argus Motoren-Gesellschaft, where
Dr Fritz Gosslau and his team began to develop a
pulse-jet engine from first principles. They were not
SURFACE-TO-SURFACE MISSILES
Above: The flying bombs were delivered to the launch
sites dismantled, but it was a simple process to assemble
them. Here the VTs wings are being introduced over the
tubular main spar.
permitted to see Schmidt's engine until March 1940;
they adopted his valve system in part, but mostly
stuck with their own design. By the end of the year,
they had produced a small engine of 150kg (3301b)
static thrust, and on 30 April 1941 this engine made
its first flight, beneath a Gotha Go 145 two-seater
biplane trainer. During the summer, small cargo gliders
made flights under pulse-jet power alone, which
validated the concept, but it was a further year before
the RLM took the next step, and on 19 June 1942,

SURFACE-TO-SURFACE MISSILES
Above: V1s were launched on ramps by steam catapults.
When they reached around 400km/h (250mph), their own
powerplants took over and the guidance system took them
in a gentle climb to their cruising altitude.
ordered Gerhard Fieseler to begin developing an airframe
for a flying bomb. In the meantime Argus carried
on developing the powerplant, Walter began work
on a catapult launching system, and Siemens set out
to produce a guidance system using an existing
autopilot as a basis.
The airframe was actually the work of Robert
Lusser who, we may recall, was involved in the original
P. 1065 project at Messerschmitt, and Willy
Fiedler. Development took 18 months, and it was
early December of 1942 before the first (unpowered)
example was launched from an Fw 200 'Condor' over
the test range at Peenemiinde-West, to be followed by
the first catapult launch on Christmas Eve. In one
form or another, a total of perhaps 350 missiles were
expended in the course of testing. At the start, testing
did not proceed smoothly. The situation was complicated
by the necessity to test all the components
together, which made fault isolation difficult, but
64
eventually the design of the air intake and the fuelsupply
system were identified as the seats of the worst
problems, and when they were re-thought, the bomb
flew much more reliably. However, it flew considerably
more slowly than had been envisioned, at around
600km/h (370mph), which made it vulnerable to
interception by existing fighter aircraft. Consequently,
there was a non-stop programme to improve the Vl's
performance, both by upping the output of the Argus
109-014 motor (by injecting nitrous oxide into the
combustion chamber, for example) and by replacing it
with a more powerful unit such as the 109-044 or the
Porsche 109-005 turbojet - both of which produced
500kg (1 lOOlb) of static thrust - or by an unspecified
ramjet. By the war's end, experimental models were
flying at almost 800km/h (500mph). By then, they
were faced with much faster interceptors, such as the
jet-powered Gloster 'Meteor' which scored its first
combat victory on 4 August 1944 when it destroyed a
VI by tipping it over with its wingtip to destabilise it.
This was not as risky a manoeuvre as one might think,
and was deemed preferable to shooting the flying
bombs down at close range, with the attendant risk of
damage to one's own aircraft. In fact, the Vis were a
much easier target for guns on the ground than they
were for aircraft, since they flew straight and level and
at a fixed speed; more were destroyed by this means
than by any other.
DESIGN MODIFICATIONS
Not entirely surprisingly, the guidance system and its
installation proved to be problematic, too. The first
difficulty actually showed up before the Fi 103 airframe
was completed, and involved the positioning of
the engine vis-ä-vis the fuselage. Tests carried out
with engines mounted on Do 17 and Ju 88 aircraft
showed that the pulse action produced considerable
vibration, particularly if the exhaust stream passed
over the fuselage, and so the design was modified to
move the entire engine aft so that it overhung the tail
by some considerable extent. Close attention had to
be paid to the mountings, and eventually a system was
adopted which combined a pivoted yoke at the front
secured with a single pinned lug to the tail fin, both of
the mountings in rubber bushes. However, there were
still problems with vibration. The guidance system
itself relied on a gyroscope for control in all three
axes, linked to a master compass set to the desired
heading before launch for azimuth control, and an
aneroid barometer for altitude control. Corrections
were transmitted to the servo-motors acting on the

udder and elevators by means of compressed air. The
distance flown was computed by means of an air-log
driven by a small airscrew in the nosecone, and when
a predetermined figure had been reached, a pair of
detonators exploded, locking the elevator and rudder
and deploying two spoilers, forcing the aircraft into a
dive. This somewhat complicated procedure was necessary
because the temperature in the jet pipe was
high enough, even after just a few seconds' running,
to sustain ignition alone, as there was no critical timing
to worry about, and so the rather simpler method
of cutting the current to the spark plug would have
had no effect. It would perhaps have been possible to
cut the fuel supply instead, though since the fuel system
was pressurised this was not entirely predictable
SURFACE-TO-SURFACE MISSILES
either, and in any event, it was actually more desirable
for the vehicle to go into a powered dive. For some
time the fuel did tend to cut out as the VI tipped over.
This was not a feature, but a fault which was eventually
corrected.
The bomb was equipped with three different types
of fuze: an electrical impact fuze, powered by an onboard
battery and with a resistor/condenser circuit
which held enough charge to detonate the device if
the battery connection was severed on impact; an
Below: Since V1s flew at a constant speed, at constant
height and on a straight course, it was relatively simple
for anti-aircraft gunners to establish a box barrage,
particularly at night when the jet flare was obvious.
65

SURFACE-TO-SURFACE MISSILES
Above: The preferred way to destroy the bombs from the
air was to tip them off course - not as risky a business as
one might suppose. The aircraft pictured in this gun
camera shot is, from its wingform, a Spitfire.
electro-mechanical all-ways fuze with a trembler
switch; and a mechanical (clockwork) delayed fuze.
The impact fuze had three actuators: one in the nose
and one in the belly (both of which functioned by
pressure); and an inertial switch in the fuze itself. The
fuzing system was so good that of the first 2500 to hit
the UK, only four failed to go off.
The launch system was less problematical than
other elements, and employed a simple steam catapult,
the steam being generated by the reaction of the
same T-Stoff and Z-Stoff (basically hydrogen peroxide
and calcium or potassium permanganate, as we
might recall) used in rocket motors. The catapult track
was a slotted tube 42m (138ft) long, inclined at an
angle of six and a half degrees (later, a track half that
length was employed), on a concrete and steel bed,
within which a dumbell-shaped free piston ran. The
piston incorporated a fin which protruded through the
slot in the tube, and engaged with a simple trolley on
66
which the missile sat. The slot was sealed by a tubular
strip which trailed behind the piston to be forced
into the slot by the pressure of the steam. The fuel to
generate the steam was contained in tanks on a trolley,
which also held the forged steel steam generation
chamber, secured to the rear of the launch tube by a
bayonet fitting. Alongside the rear of the ramp, there
was a starter unit which contained the equipment necessary
to get the pulse-jet operating.
LAUNCHING THE V1
The launch procedure was straightforward. The pulse
jet was fired up and allowed to run for seven seconds,
bringing it up to the correct operating temperature.
The valve on a large bottle of compressed air was then
opened by remote control, forcing 60 litres (13.2 gallons)
of T-Stoff and 5 litres (1.09 gallons) of Z-Stoff
into the steam generation vessel. Their reaction generated
a large volume of super-heated steam, and as
soon as the pressure in the chamber built up sufficiently,
a restraining bolt sheared, whereupon the piston
was free to travel up the tube, carrying launch
trolley and missile with it. By the time it reached the
end of the track - little more than half a second later,

having been accelerated at a rate of around 16 g - the
whole assembly was travelling at around 400km/h
(25()mph) and the pulse-jet had started to run independently.
The piston was literally fired out of the
tube and fell to earth some distance away (along with
the launch trolley) to be recovered later, while the flying
bomb began its climb to operational height at a
rate of about 150m (492ft) per minute. The guidance
system corrected its course as it went, and the aneroid
capsule reset the elevators for level flight when the
pre-determined altitude was reached.
The Fieseler Fi 103 A-1, the original and technically
most common version of the flying bomb, was
about 8m (26ft) long. Its wingspan was of around 5m
(17ft) although there were two different wings produced
in slightly different form and dimensions, and
it had a maximum fuselage diameter of 0.84m
(2.75ft); the warhead comprised 830kg (18321b) of
Trialen (amatol), which was sometimes supplemented
SURFACE-TO-SURFACE SSILES
by incendiary bombs. Provision was made to replace
the explosive with gas, though this never happened in
practice. A full load of 75-80 octane fuel added
515kg (11331b) to the all-up launch weight total of
2180kg (48061b). It had an autonomous range of
240km (150 miles) at a maximum speed of 645km/h
(400mph), and an operational ceiling of 3000m
(9800ft). It was fabricated from sheet steel pressings,
with an aluminium nosecone and sheet-steel wings
around a single tubular steel spar. The emphasis was
on keeping costs to a minimum, and little effort was
put into reducing weight by employing more exotic
materials. In 1945, the Fi 103 F-l was produced.
Basically similar to the A-l, its warhead contained
Below: Very few V1 s were recovered intact after they had
been brought down, but some failed to explode and gave
up their secrets instead. Here, RAF personnel are seen
examining one in a bean field, somewhere in Kent.
67

SURFACE-TO-SURFACE MISSILES
FIESELER Fi 103 (V1) STANDARD
MODEL
Type: Cruise missile
Length: 8.32m (27.3ft)
Span: 5.30m (17.39ft)
Launch weight: 2180kg (4806lb)
Above: The Fieseler Fi 103, to give the V1 its official name,
was unleashed in earnest against England in Operation
Boxroom, which began in June 1944.
436kg (9621b) of amatol, and its fuel tanks were
enlarged from 568 litres (125 gallons) to 756 litres
(166 gallons), increasing range to 370km (230 miles).
THE V1 CAMPAIGN BEGINS
The first operational Vis were launched in the early
hours of 13 June 1944. Just 10 missiles were
deployed: four crashed immediately; two fell into the
sea; and four hit the Home Counties (one in Sussex,
one near Sevenoaks in Kent, one in the south-eastern
suburbs of London, and one in Bethnal Green, north
of the Thames). Two days later, Unternehmen
Rumpelkammer (Operation Boxroom) commenced in
earnest, and between 2200 hours on 15 June and 12
noon the following day, 244 Vis were launched, most
of them against London and some against Southampton
which was the re-supply base for the invasion
force, even then trying to fight its way out of the
beachhead in Normandy. More than half of the flying
bombs launched (144 in all) crossed the English
coast, and 34 were shot down by anti-aircraft guns
and fighter aircraft.
This campaign from launch sites in the Pas de
Calais continued until the end of August, by which
time Allied troops were closing in. The Luftwaffe's
Flakregiment 155 (W), its name a cover like the FZG
76 designation, had been set up in August 1943 under
the command of Colonel Max Wachtel, and it packed
up and moved to Holland with the intention of concentrating
activities on Antwerp. By that time, it had
launched 9017 missiles, 6725 of which had reached
England. As many as 2340 landed in the Greater Lon-
68
Max speed (later models): 800km/h (497mph)
Range: 240km (150 miles)
Warhead: 830kg (1832lb) of amatol
don area, the vast majority of them exploding as
planned. Other reports suggest that 8892 missiles
were launched with the UK as their target during the
entire war, and still others put the total at fractionally
over 10,000. As early as 7 July, the ground launches
had been supplemented by air launches from Heinkel
He 111 bombers of HI/KG 3, based at Gilze Rijen in
Holland, which carried one missile each on a pylon
located just outboard of the starboard wing root, and
launched it at an altitude of 450m (1500ft) over the
North Sea. By the end of August, over 400 missiles
had been deployed in this way, mostly against London,
but some against Southampton and Bristol.
Air-launched operations against targets in the
United Kingdom recommenced in mid-September in
a campaign which lasted until mid-January. A total of
around 1200 missiles were launched (some of them at
targets as far north as Manchester, though only one
reached that particular objective), but only around 20
per cent of them got through to populated areas and
just 66 landed on London, still the prime target in the
UK. During the same period, around 1600 missiles
were air-launched against Antwerp and Brussels. In
all, they cost the Luftwaffe 80 aircraft shot down.
On 3 March 1945, a new campaign against London
started from sites in Holland, using F-l missiles with
greater fuel capacity and a smaller warhead, but this
was of only very limited success. The last flying
bomb landed in London on 29 March. In all, a total of
2419 Vis had hit London and 2448 had struck
Antwerp (though these were not the only targets, of
course), representing roughly 25 per cent of those
launched. It is estimated that VI rockets were responsible
for the deaths of perhaps 12,000 people. Official
figures put the death toll in the UK at 6184, with
17,981 injured. Altogether, around 34,000 Vis were

produced, by Fieseler, Volkswagen (initially with a
marked lack of success), and 'Mittelwerke', the
underground factory at Nordhausen in the Harz
mountains staffed almost exclusively by slave labour.
The V1 was very cost-effective, even if it was at best
only 20 per cent effective. Estimates of the unit cost
vary, but around 5000 Reichsmarks seems reasonable
at a time when the standard German infantry rifle, the
Mauser 98K, was costing RM56, and a PzKpfw IV
tank over RM 100,000.
YOKOSUKA MXY7 'OHKA'
Type: Single-seat suicide missile
Length: 6.066m (19.9ft)
Span: 5.12m (16.8ft)
Max take-off weight: 2140kg (4718lb)
SURFACE-TO-SURFACE MISSILES
Above: The Reichenberg IV, seen here, was the
operational version of the manned flying bomb, with a
warhead but without the landing skid on its belly or flaps
on the trailing surface of the wings. None was ever flown
in combat.
Below: The Japanese Navy also worked on a manned
flying bomb, the Yokosuka MXY7 'Ohka'. Simpler than the
Reichenberg, it had rocket boosters to accelerate its
gliding attack and only rudimentary flight controls.
Max speed: 649km/h (403mph) at 3500m
(11,482ft)
Range: 37km (23 miles)
Warhead: 1200kg (2646lb) of explosives

Left: A complete VI weighed some 2.032 tonnes (2 tons),
and it was customary to manhandle it into position at the
foot of the ramp on its launch cradle.
THE SELBSTOPFERMÄNNER BOMBER
Desperate times breed desperate men, and both
remaining arms of the Axis began to consider formalised
suicide tactics, perhaps from as early as late
1943. The most famous of these was the Japanese
Kamikaze (Divine Wind) campaign against ships of
the Royal and US Navies from the time of the Battle
of Leyte Gulf (23-26 October 1944), but Germany,
too, made preparations for the use of such tactics, the
most significant of those involving a manned version
of the Fi 103 flying bomb. This was actually the first
vehicle considered, but it was rejected in favour of a
glider version of the Me 328, while a unit equipped
with Fw 190s, known as 'Kommando Lange 1 , or the
'Staffel Leonidas', was formed to begin training for
missions which involved the pilot placing his aircraft
- carrying the maximum possible bombload - in a
steep dive aimed at the target before baling out and
taking to his parachute. Eventually, the Me 328 project
lost momentum, and it became clear that the
chances of penetrating anti-aircraft defences in a Fw
190 carrying a sufficient bombload to be effective
were extremely slim.
Attention returned to the use of the Fi 103. Designs
for four different versions were worked up by DPS,
and Henschel converted four standard VI missiles.
The operational codename for the project was
'Reichenberg', and the four versions of the aircraft
received 'R' prefixes, I through to IV. The Fi 103 R-I
was a single-seater with ballast in place of its warhead;
it had skids and landing flaps, but no motor: it
was constructed for the test programme. The R-II was
similar, but with a second cockpit in the nose section.
The R-III was designed for advanced training, and
was essentially the R-I equipped with an engine. The
R-IV was the operational model, with no landing aids
but with ailerons, and with the warhead reinstated.
There are suggestions that the warhead might have
been replaced with a cannon and the aircraft used as
an interceptor, too. About 175 are thought to have
been built in all.
The test pilots for the development programme
were Heinz Kensche and the ubiquitous Hanna
Reitsch, and they reported favourably on the aircraft's
performance in flight (though there were hair-raising
moments, apparently) but were not so enthusiastic
about landing it. One can imagine that landing was
SURFACE-TO-SURFACE MISSILES
hardly a consideration as these aircraft were never
meant to be landed after use, except on training
flights. The intention was for the pilot to aim the aircraft
at its target and then bale out, but frankly, the
arrangements made for him (or her) to exit the aircraft
were somewhat cynical. The cockpit was located well
aft - aft of the trailing edge of the wings - and almost
underneath the motor's air intake, against which it
jammed before it had been opened through the 45
degrees necessary to jettison it. Even if the pilot succeeded
in freeing it, he would have had little chance
of levering himself out of the cockpit in a steep dive
at speeds in excess of 1000km/h (62()mph) without
being seriously injured, if not killed. Although thousands
volunteered for the Selbstopfermänner bomber
programme and 70 were accepted for training, they
were never asked to go into action, so in the final analysis,
it is not important. Japanese pilots who flew the
'Ohka' flying bombs in the latter stages of the
Kamikaze campaign were treated more honestly: they
were sealed into their aircraft and knew they had no
chance of getting out. The efficacy of the Japanese
Kamikaze campaign gives some indication of the sort
of results they were expected to achieve. Between 21
February and 15 August 1945,17 ships were sunk and
198 damaged for the loss of 930 aircraft, both flying
bombs and escorts.
THE'AGGREGAT'ROCKETS
In the aftermath of the defeat of 1918, Germany was
severely limited in terms of the weapons she could
possess. As we noted earlier, there was a large-scale
campaign to circumvent the restrictions imposed by
the Treaty of Versailles by establishing development
programmes abroad, but there were other avenues
open, too; for instance, as early as 1929, the
Heereswaffenamt began to look into rocketry as an
alternative to long-range artillery, and set up a trials
and proving ground about 32km (20 miles) south of
Berlin at Kummersdorf. Captain Walter Dornberger, a
professional soldier who had been sent by the Army
to the School of Technology at Charlottenberg, and
had earned an MA in ballistics there, was put in
charge of the project in 1930 under the HWA's head,
Karl Becker, himself very enthusiastic.
In 1927, a group of keen amateurs, centred on Hermann
Oberth, author of Die Rakete zu den Planetenräumen
(The Rocket into Interplanetary Space), published
in 1923, formed the Society for Space Travel,
the Verein für Raumschiffahrt. They began to experiment
with rocket motors, and were funded initially by

SURFACE-TO-SURFACE MISSILES
Fritz von Opel (who, we may recall, had commissioned
a rocket-powered glider from Alexander Lippisch,
and had also built a rocket-assisted car, the
RAK 2), and funded latterly by a 10,000-franc prize
Oberth won in 1929 for his book Wege zur Raumschiffahrt
(Ways to Spaceflight). In 1930, a promising
student named Wernher von Braun joined the Society
and the following year, they successfully flew a small
rocket fuelled by liquid oxygen and petrol. By then,
funds were running short, but fortuitously, the Society
was approached by Dornberger, who arranged for
them to receive a series of small grants. In 1932, von
Braun, just graduated from the Berlin Technical Institute
with a BSc in mechanical engineering, went to
72
Above: The launch pad at the Peenemünde research
station, deep in the pine forests of the island of Usedom
on the remote Baltic coast. All the test flights of the A4
were initiated from this site.
work at Kummersdorf and by December 1934, his
group had launched two liquid-oxygen- and alcoholfuelled
rockets, designated A2, which had reached
altitudes of over 2500m (8200ft).
In 1935, work started on a new rocket, the A3,
which weighed 750kg (16551b) and stood 7.6m (25ft)
tall. It, too, was fuelled by A-Stoff (liquid oxygen, at
-183 degrees C) and M-Stoff (methyl alcohol, or
methanol), but this time the motor produced 1500kg

Right: A technician is photographed making last-minute
adjustments to the guidance system prior to launching an
A4 rocket, which has been brought to the vertical position
by the mobile erector.
(33001b) of thrust for 45 seconds instead of the 300kg
(6601b) for 16 seconds of the A2. More important,
perhaps, was the new method of stabilisation which
von Braun's team devised. Whereas the A2 was stabilised
by its centre section being spun by an electric
motor to create a gyroscopic effect, the A3 would
have small molybdenum 'rudders' (more accurately,
vanes) acting to deflect a portion of the exhaust
stream under the control of gyroscopes. The A3 also
had four rudimentary tail fins, though these hardly
extended outside the diameter of the body. Its payload
consisted of an instrumentation package, and it was to
return to earth on a parachute. The first A3 launch
took place on 6 December 1937 from the island of
Greifswalder Oie, off the Baltic coast. The new stabilisers
worked, but other elements of the design, in
particular the overall aerodynamics, were faulty, and
the rocket was never entirely a success, although three
examples were launched.
THEMOVETOPEENEMUNDE
By then, the research group was fast outgrowing the
facilities at Kummersdorf. The A2s were actually
launched from the island of Borkum, off the mouth of
the River Ems in the North Sea. In early 1936, the
HWA and the RLM joined forces to purchase a large
area of suitable land, an isolated peninsula around the
village of Peenemünde on the island of Usedom, off
the Baltic coast close to the present-day border with
Poland. They also bought the adjacent Greifswalder
Oie, and it was to this location that both moved their
rocket development programmes. The Army were
located to the east of the site, in an area known as
Heeresversuchsanstalt-Peenemünde (HVP), and
referred to as Electromechanische Werke (EMW) as a
cover, where Dornberger was appointed Head of
Weapon Test Section 11, with von Braun as his Technical
Director. It was here that the first successful ballistic
missiles the world had ever seen were developed
and tested, and the name Peenemünde soon took on a
new significance.
After the failure of the A3 to live up to expectations,
development work on the A4, which was
always intended to be a military rocket, was halted.
Instead, von Braun turned to the design of another
research rocket, the A5, somewhat larger than the A3
SURFACE-TO-SURFACE MISSILES

SURFACE-TO-SURFACE MISSILES
but with the same motor. The main difference
between these and the earlier design was to be in the
profile of its flight path, because now the requirement
was not simply to send a rocket straight up into the
atmosphere, but to launch it at a terrestrial target hundreds
of kilometres away, and for that, a sophisticated
guidance package was required. In the case of a small
device like the V1, basic direction was simply a matter
of aligning the launch ramp with the azimuth of
the target, and then relying on a gyrocompass to apply
small corrections. But steering the ballistic missile to
its target would be quite another matter, since it would
have to be launched vertically, and then tipped over in
the precise direction of the target to an angle of 41
degrees from the horizontal and maintained there.
Range was determined by the length of the burn, and
that meant that propellant cut-off had to be precise
and instantaneous. Cut-off was actuated initially by a
radio signal from the ground, and was the only external
factor applied after the launch sequence had been
initiated (and this, too, being later automated). With-
Below: The RAF launched a major raid on Peenmünde on
the night of 17/18 August 1943, and caused considerable
damage, particularly to accommodation blocks. Both
slave labourers and research staff died in the raid.
74
out going too far into the intricacies of the matter, to
achieve a proper degree of directional stability in a
ballistic missile it is necessary to be able to control its
movement in three axes: pitch (to achieve and maintain
the proper angle of climb); yaw (side-to-side
movement, to correct the heading); and spin, which is
a natural tendency of a cylindrical body in motion, but
which makes controlling pitch and yaw by means of
rudders almost impossible, and which must be
damped out. To make matters worse, the characteristics
of the missile - in particular the all-important
centre of gravity - change as its fuel is consumed, and
its flight characteristics change no less drastically as it
climbs into and through the upper atmosphere and
then descends again on its parabolic course.
EPOCH-MAKING RESEARCH
All in all, the problems of guidance were the most
complex Wernher von Braun's team had to face, and
they solved them definitively and, we may add, with
nothing more sophisticated than slide-rules and
mechanical calculators; it is perhaps significant that
some of the first simple computers were produced to
solve ballistic problems. The team used three-axis
gyroscopes controlling small rudders built into the
tips of the fins, supplemented by deflector vanes,

made now of graphite rather than molybdenum, in the
exhaust stream during the first few seconds of flight,
when the airflow over the conventional control surfaces
was insufficient. The team's work on the remote
north coast of Germany under increasingly difficult
conditions between 1938 and 1945 was actually to
change civilisation itself - if not in the sense that at
least some of them intended - by enabling man to
leave earth for the first time.
During 1938, work proceeded on the new design,
and by the year's end, four unguided launches had
been made to a distance of 17km (10.6 miles), and an
altitude of 11,000m (36,000ft). Work on the guidance
system continued. By October 1939, a month or so
into World War II, the guidance and control package
- in fact, every essential component of the A4 except
its warhead and motor - had been assembled in the
rocket, and test firing commenced. The results were
successful, and in early 1940 Dornberger thankfully
ordered work on the A4 to begin once again, with a
production target date of mid-1943. He bargained
without Adolf Hitler.
SURFACE-TO-SURFACE MISSILES
Above: Many of the A4s captured intact found their way
to the United States (as did most of the development
team). This A4 is being readied for launch, probably at the
White Sands Proving Ground, New Mexico.
By July 1940, it seemed that Hitler's war would be
over by the year's end, with virtually all of Europe
under his control, the Soviet Union pacified by treaty,
and Britain isolated. It was then that the Führer gave
the fateful order to cancel any research project which
could not be guaranteed to show results within 12
months. One of the first casualties was Dornberger's
war rocket. Or so, at any rate, went the theory. In fact,
Dornberger managed to evade the directive by continuing
to work on individual components, including the
25,000kg- (55,1251b-) thrust engine, and was also
able to continue the A5 programme, which was still
supplying much-needed data on flight characteristics.
In fact, test firings of the new motor, the brainchild
of Dr Walter Thiel, had already begun. These tests had
revealed that there would be additional problems in its
operation, relating purely to scale, particularly in

SURFACE-TO-SURFACE MISSILES
76

cooling it and supplying it with sufficient fuel. The
calculations had shown that to obtain 'the required
thrust, it would be necessary to deliver almost 125kg
(2751b) of fuel to the combustion chamber every second.
The earlier rockets had required very much less,
and it had been sufficient to pressurise the propellant
tanks with nitrogen. But now it was necessary to
devise a means of actually pumping the fuel and the
liquid oxygen from tank to burner. The method chosen
was a steam turbine, and the means of generating
the steam was the same as that used in the Vl's launch
catapult: the near-explosive decomposition of T-Stoff
into super-heated steam when it came into contact
with the catalyst Z-Stoff. The turbine thus powered
produced around 675hp and ran at 500()rpm.
TO THE MARGINS OF SPACE
Thanks to a long catalogue of setbacks (and, we may
imagine, the need to keep the project at least partially
hidden from those who would have preferred more
resources to have gone into their own laboratories),
the hand-built prototype A4 was not ready for static
testing until 18 March 1942, and even then, it exploded.
Von Braun's team built another one, which
exploded too, but eventually they managed to make
enough progress to dare a test flight. Scheduled for 13
June, it was a failure. Von Braun returned if not to the
drawing board, at least to the workshop, and readied
another prototype. After a second failed test launch,
on 16 August, happily for von Braun and Dornberger,
the third attempt on 3 October proved more successful.
The missile flew over 200km (125 miles) to an
altitude of 85km (53 miles) and thus into the ionosphere
at the margins of space; it returned to earth
within 4km (2.5 miles) of its intended target. Now all
that remained was to sell the concept as a weapon of
war; by late 1942 that was not much of a problem.
Hitler endorsed the V2 programme, as it soon
became known, on 22 December, It was held up by
shortages of strategic materials and by the RAF,
which sent a mixed force of 596 aircraft to drop 1828
tonnes (1800 tons) of bombs on Peenemünde on the
night of 17 August, losing 40 aircraft and killing
around 800 people on the ground - most of them conscripted
Polish labourers, but including Dr Thiel -
and setting back the programme by perhaps two
Left: Some captured A4 rockets were launched from sites
in Germany into the German test target zones. Here,
British personnel prepare to launch a V2 using the original
equipment, including the 'Meillerwagen' erector/launcher.
SURFACE-TO-SURFACE MISSILES
months. It had seemed for a while that the Armysponsored
A4 would lose out to the Air Force's Fi
103, but a demonstration of both before high-ranking
government officials in May 1943 came at a bad time
for the latter, and the A4 programme survived. As the
war situation worsened that year, Hitler became more
and more interested in the A4, eventually giving it the
highest priority, allocating production facilities at one
of Henschel's factories and at the Zeppelin works at
Friedrichshafen. Both sites were bombed before production
could start up, in fact, and A4s were instead
assembled at the 'Mittelwerke' underground factory
at Nordhausen from components manufactured all
over occupied Europe. First deliveries were made in
July 1944, and from September, the month when the
V2 campaign started, a steady output of over 600 a
month was maintained. Meanwhile, a training and test
unit was established and launch sites were selected.
There were two opposing views as to how the V2s
should be deployed. The Oberkommando des Heeres
(OK.H - Army High Command) wanted huge, wellprotected
fixed sites, and selected three locations in
Northern France from which rockets could be
launched against England. The first of these, at Watten,
near St Omer, was destroyed by the USAAF on
27 August 1943 while construction was still in an
early phase; the second, at Siracourt, and the third, in
a quarry at Wizernes, were truly massive affairs, over
one million tonnes (one million tons) of reinforced
concrete being cast into a protective dome, beneath
which storage and launch chambers, and accommodation,
were hollowed out. They were both destroyed
by the RAF in July 1944 as part of Operation Crossbow
(the broader campaign to destroy the VI launch
sites) using 'Tallboy' penetration bombs, and finished
off with remotely controlled B-17 Flying Fortresses,
packed with explosive, the following month. With
that, the thoughts of the high command turned to the
sort of mobile launchers that Dornberger had been
advocating all along.
30-VEHICLE BATTERY
Given the complexity of the missile itself, the launch
procedure was quite straightforward. One of the
trucks in the battery's 30-vehicle convoy carried a circular
launch platform fabricated from steel, which
incorporated a blast deflector. This was set up on the
ground at the rear of the missile transporter and levelled
by means of screw jacks in its four legs. TheFR-
Anhanger-S missile transporter, commonly known as
the 'Meillerwagen' after its manufacturer, was

SURFACE-TO-SURFACE MISSILES
secured to it. While the power and test cables were
being run out from the generator and control trucks,
two of the three straps retaining the missile on its
trailer bed were removed, leaving the topmost in
place, and the nose fuze was then inserted. An auxiliary
motor provided power for the hydraulic rams
which then raised the missile to the vertical position -
a process which took about 12 minutes - and when it
was hanging vertically over the launch platform, the
latter was jacked up to take the missile's weight and
the top retaining strap was removed.
The various cables were then connected up, the
transporter withdrew a short distance so that hinged
platforms on its gantry could be deployed as work stations,
and the testing procedure began. Once this had
been successfully completed, the fuelling crews went
to work, filling the main tanks with liquid oxygen and
methanol and the smaller tanks with hydrogen peroxide
and the permanganate catalyst. Then the launch
78
platform was rotated on its base to align the missile
with the target (the process of tipping it in flight was
carried out by spinning a drum around its horizontal
axis, thus causing the missile to rotate slowly in the
opposite direction; the axis of the drum had, therefore,
to be precisely at right-angles to the azimuth of
the target). Lastly, the igniter - a small firework, set
off electrically - was wedged into the tail pipe, and
the set-up crews withdrew.
Right: In addition to the 'Meillerwagen' and its fleet of
associated vehicles, A4 launch teams also employed
special trains. They were somewhat less flexible
logistically but smoother in operation.
Below: The A4 rocket - even without its 975kg (2150lb)
warhead filled with amatol mix- could make a very large
hole in the ground indeed... This crater was the result of
a test firing at White Sands.

SURFACE-TO-SURFACE MISSILES

SURFACE-TO-SURFACE MISSILES
The armoured launch control booth was situated in
the back of a half-track vehicle, based on either the
SdKfV, 11 Leichter Zugkraftwagen or the similar
SdKfz 251 Mittlerer Schützenpanzerwagen, the
armoured maid-of-all-work of the German Army
since 1944. Closing the firing switch opened the
valves in the T-Stoff and Z-Stoff tanks and set the turbine
pump in motion. Once it was up to speed, the
main valves were opened, feeding propellant to the
combustion chamber, and the igniter was fired. Directional
control in the first few seconds was achieved by
the carbon vanes in the exhaust gas flow, but as the
rocket's speed increased, the external fin-tip rudders
took over. As the missile rose, the spin of the drum
caused it to tip over slowly, and at the appropriate
point, the propellant supply was cut, initially by radio
signal, later by command from an accelerometer. The
warhead was armed only during flight, about 60 seconds
after lift-off at the moment of propellant cut-off,
Below: As this cutaway diagram shows, most of the
internal volume of the A4 was taken up with tanks
containing the liquid oxygen and methanol it used as fuel.
80
PEENEMUNDEA4 (V2)
Type: Long-range ballistic missile
Length: 14.05m (46.09ft)
Diameter: 1.68m (5.51ft)
Lift-off weight: 12,870kg (28,373lb)
Speed: 5580km/h (3465mph)
Max range: 330km (205 miles)
Warhead: 975kg (2150lb) of amatol mix
and there was an interlock in the arming system
which prevented arming taking place if the right conditions
were not met. There was no provision for
destroying the missile in flight on command.
TARGET PARIS
There were five batteries in all, based around the
Hague in Holland - one from Artillerie Abteilung
(AA) 444, two from AA 485 and two from AA 836.
The first and last formed the Southern Group, and
operated against targets in France and Belgium, while
AA 485 formed the Northern Group and was tasked
with targeting England. Tt was AA 444 which
launched the first operational V2, against Paris on 5
September 1944. Three days later, AA 485 fired two
rockets aimed at London, the first of which hit Staveley
Road, Chiswick, in west London - having been
aimed at Southwark, 13km (8 miles) away - at just
before 1845 hours in the evening, demolishing six
houses, killing three people and injuring 17. The campaign
against London was to last exactly 200 days,
the last missile falling at 1920 hours on 27 March
1945, hitting a block of flats in Whitechapel, killing

134. Other reports suggest that the last A4 launched
against London actually fell in Orpington, Kent, that
day. In those 200 days, out of 1120 launched, 1054
rockets landed in England, 517 of them in the Greater
London area, and, according to official figures, killed
2754 people and injured 6532. The larger Southern
Group fired rather more missiles in all (about 1675),
most of them targeted against Antwerp (1341). It also
directed its fire against Brussels, Liege, Luxembourg,
Paris and the Rhine crossing at Remagen. There was,
of course, no defence against the V2. Only the Allied
advance across northern Europe, which drove the
Mobile Artillery Battalions out of range of worthwhile
targets, put a stop to the campaign. Gruppe
Nord reportedly still had 60 unexpended missiles
when it fell back into Germany on 29 March.
It is worth noting that a project aimed at firing an
A4 from a submerged U-boat (actually, from a selfcontained
chamber it towed behind it, which was
caused to float vertically by means of flooding its tail
section) had reached a fairly advanced stage by 1945,
with several containers having been completed and
tested at the Vulkan shipyard in Stettin. Known as
SURFACE-TO-SURFACE MISSILES
Project Test-Stand XII, and conceived apparently by
Volkswagen in late 1944, this was aimed at the bombardment
of New York. However, it is suggested that
a more-or-less successful test firing in the Baltic made
it clear that a fully fuelled missile (there was no way
it could be fuelled at sea) could not be expected to
stand up to the rigours of a trans-Atlantic voyage,
even submerged. The project was shelved.
The A4 missile in its final form was to be made
entirely of steel. At just over 14m (46ft) long, with a
maximum body diameter of 1.68m (5.5ft) and a span
over its fins of 3.5m (11.5ft), it weighed 12,870kg
(28,3731b), of which 975kg (21501b) of amatol comprised
its warhead, and 4900kg (10,7801b) of liquid
oxygen and 3770kg (83001b) of methanol comprised
the bulk of its propellant. It had a maximum range of
330km (205 miles), which it covered in 3 minutes 40
seconds (of which it was under power for 70 seconds),
reaching a maximum velocity of 5580km/h
(3465mph) and height of 96,000m (315,000ft). Its
velocity at impact was 2900km/h (1800 mph). There
are rather divergent figures for total A4 production,
estimates ranging from 6000 to as many as 10,000.

SURFACE-TO-SURFACE MISSILES
Above: An A4 rocket, shrouded in tarpaulin, on the railway
flatcar used to transport it to the vicinity of the launch site.
The Allied advance across northern Europe drove the V2
battalions out of effective range of worthwhile targets.
THE LATER GUIDED BALLISTIC MISSILE PROJECTS
As soon as the A4 was viable, the project was taken
out of von Braun's hands. He and his team, it is suggested,
were never entirely satisfied with it, and
would happily have gone on refining their design, but
Heinrich Himmler, who had previously seized control
of all the secret weapons programmes, would not
accept that. Von Braun turned to working on ways of
increasing its range. The simplest means, he concluded,
was to fit it with wings, so that it would glide in
the final phase of its flight, prolonging its descent and
increasing its range to 435km (270 miles), but he
counted without the effects of re-entering the dense
air at lower atmospheric levels. The one A4b missile
which was launched successfully (the first one
crashed soon after take-off) failed to re-enter cleanly
and was destroyed.
The A6, which never made it past the discussion
stage, was to have been an A4 fueled by SV-StoiT,
made up of 94 per cent nitric acid and 6 per cent
nitrous oxide, and Visol (the generic name given to a
group of isobutyl-vinyl esters); it was to have 20 per
82
cent more thrust. The A7 was a winged version of the
A5, air-launched as a concept vehicle for the A9. The
A8 was virtually identical to the A6 but fuelled with
SV-Stoff and diesel oil, although it is also suggested
that it was to have been fuelled with LOX and
methanol contained in pressurized tanks, rather than
employing the turbine pump to deliver them to the
combustion chamber. The A9 was the A4b with modified
wing planform: essentially, the horizontal fins
were to have been continued forward, right to the
rocket's nose, in a simple ogive, to allow it to survive
re-entry; it had the motor from the A6, with a projected
range of 600km (370 miles).
The final ballistic missile project, the A10, was
much more ambitious in scale and had it ever materialised,
would have been the first ever ICBM. The projected
inter-continental ballistic missile was to have
been a two-stage rocket, the first stage being based on
six A4 motors linked into a common venturi, and
designed to propel its second stage - either an A4 or
an A9 - to an altitude of 24km (14.9 miles) before its
own motor was fired, giving it a range of around
4800km (2800 miles) with a 1000kg (22001b) amatol
warhead and a flight time of around 45 minutes. It is
suggested that this project was first discussed as early
as 1940, long before the United States entered the
war, but there is no evidence that it got beyond the

discussion stage. There was also talk of modifying the
second-stage A9 missile to carry a pilot, who would
have been ejected once he had locked the missile on a
course for its target (presumably he would have been
recovered by a submarine), but that idea can be dismissed
as a flight of fancy.
THE 'RHEINBOTE' ROCKET
The FZG 76 and the A4 were the only guided surfaceto-surface
missiles employed by either side during
World War IT, but the A4 was by no means the only
war rocket. Most of the combatant nations employed
much simpler devices - unguided and with solid-fuel
'motors' - as adjuncts to their artillery or as assault
weapons, but once again, only Germany went one
stage further, and produced a long-range unguided
ballistic missile, the Rh.Z.61/9 'Rheinbote' ('Rhine
Messenger'), developed by a company better known
for its artillery pieces and its share in the development
of the superlative MG 42 general-purpose machine
gun, Rheinmetall-Borsig. Where the A4 was complex
and expensive, 'Rheinbote' was simple. It was a finstabilised
four-stage solid-fuel rocket, each of the first
SURFACE-TO-SURFACE MISSILES
three stages igniting the next as it burned out and fell
away, with no guidance system, but relying on simple
alignment of the launch rail with the target. The
launch rail could be mounted on either a high-angle
8.8cm anti-aircraft gun mount or on a modified
'Meillerwagen', and the complete missile was almost
11.5m (37.5ft) long with a maximum body diameter
(in the first stage) of 535mm (21.1in) and a maximum
fin span of 1.49m (58.5in). It weighed a total of
1715kg (37751b), almost a third of which was propellant.
It had a maximum range of 220km (140 miles)
when fired at an elevation of 65 degrees, the final
stage, with its 40kg (881b) warhead, attaining a speed
of Mach 5.5 (almost 6000km/h; 3730mph) and climbing
to a maximum altitude of 78km (48.5 miles). Over
200 of these missiles were fired at Antwerp in
November 1944.
Below: An A4 rocket is paraded through London's
Trafalgar Square in late September 1945. The rocket was
reportedly captured in France, and was later set up as if
for launch next to Nelson's Column. Greater London was
on the receiving end of more than 500 V2s in 1944-45.
83

CHAPTER SIX
Air-to-Air Weapons
While the adoption of the machine gun made air-to-air combat feasible, by the midyears
of World War II, it had come close to causing a stand-off: machine gun- (and
even cannon-) armed aircraft dared not approach each other: it was too dangerous.
The alternative, it was clear to German researchers, was to develop small rocketpropelled
flying bombs which could be directed to their targets via either wire-borne
or radio signals from a chase plane which stayed outside the lethal area.
During his post-war interrogation, Generalleutnant
Adolf Gal land described the many and various
weapons the Luftwaffe had used - or had contemplated
using - against the tightly packed formations of
Allied daylight bombers with their heavy defensive
firepower. He described how attacking the formations
from the rear immediately resulted in heavy casualties,
and how the German interceptors then switched
over to attacking them head-on, hoping to break up
the formation and then go after consequently vulnerable
individual aircraft. This worked up to a point, but
only until the bombers began taking concerted evasive
action, and from then - some time in the winter of
1942-43 - the Luftwaffe began looking at alternatives
Above: Henschel developed the Hs 293 for use against
shipping, but an air-to-air variant was also produced.
Left: Germany desperately needed an antidote to massed
formations of Allied bombers like these B-17s.
to the simple cannon and machine gun to arm their
aircraft, to allow them to attack either from unexpected
directions or from outside the effective range of the
Fortress's and Liberator's .5 inch Brownings. Because
the bombers flew so close together, much consideration
was given to bombing them, and a variety of
methods were tested, including dive-bombing individual
aircraft; towing command-detonated 10kg
(221b) fragmentation bombs on long cables (tested in
combat, with two unconfirmed successes, despite the
physical difficulty of actually delivering the weapon,
which trailed out behind the towing aircraft); and
dropping blast and fragmentation bombs on
parachutes ahead of the formation to form an aerial
minefield (this latter method was promising, but
development of a satisfactory weapon came too late).
Other methods included using forward-firing heavy
cannon - essentially, light anti-aircraft and anti-tank
guns - to shoot at them from a great distance, but this
was to prove only marginally effective; and using

Above: The simplest of all air-to-air missiles was the
unguided rocket, fired in a salvo. This Ba 349 was armed
with 24 R4M rockets with 250g (8.8oz) warheads.
obliquely firing cannon to attack them from below.
This approach was to prove devastatingly effective
against RAF night bombers, but less so against the
USAAF, whose aircraft had belly and waist gunners.
One of the reasons that heavy forward-firing guns
were ineffective was the amount of recoil they produced:
it slowed the aircraft perceptibly if more than
a few rounds were fired. The effect should not be
underestimated. One trainee in an Me 262, who found
himself committed to landing on too short a strip, let
go with the four 30mm MK 108 in the aircraft's nose
and brought his aircraft up short of the end of the runway,
thanks to the additional braking effect. Another
reason was the extra drag these usually externally
mounted guns created, reducing the aircraft's performance
considerably. For the Germans, the employment
of relatively heavy calibre guns in aircraft seems
to have had a lasting fascination. Other nations' air
forces tried it too; the ultimate in that line, according
to one source, seems to have been the fitting of a
32pdr (94mm) anti-tank gun into a Mosquito. For the
Germans, the programme to adapt light anti-aircraft
guns and anti-tank guns - notably in 3.7cm and 5cm
calibres, though 7.5cm was tested, too - continued to
the war's end. Some of the last German aircraft left in
combat were a pair of Me 262A-la/U4s with the 5cm
Mauser MK 214 mounted in the nose. One of these
aircraft, nicknamed 'Wilma Jeanne' was captured
intact by US forces, but was destroyed after it suffered
engine failure during a flight to Cherbourg, where it
was to have been loaded aboard a ship for the USA.
There was an alternative: the so-called 'recoilless
rifle', invented during World War I by an American
naval officer named Davis. A variety of recoilless
rifles were mounted on aircraft and tested, but though
the type worked well enough in principle - and one, it
is reported, was used successfully in combat - this
was a single-shot weapon, with all the problems
thereof. In fact we may bear in mind that the only reason
air-to-air combat had ever been even possible was
thanks to the machine gun, with its unique ability to
keep on throwing bullets into a target area until something
ran into one or more of them. The weapons in
question were of two basic types. The simpler type
worked on the counter-shot principle and was almost
two guns in one. The 'ordinary' barrel contained the
projectile; a subsidiary barrel behind the breech, precisely
aligned with the regular barrel, contained a
counter-shot of the same weight, usually composed of
wax or grease and lead shot in a paper cartridge. In
between them lay the chamber containing the propellant
cartridge. When the gun was fired, both projectile
and counter-shot left their respective barrels with the
same energy, and their recoils thus cancelled each
other out. In the more refined (and more complex)
version of the weapon, the cartridge case became the

counter-shot, its lesser mass being compensated for
by allowing a proportion of the propellant gases to be
exhausted through a series of jets in the chamber wall,
the components once again cancelling each other out.
Both methods worked, though the latter caused some
bad moments for pilots who flew aircraft so equipped.
THE ZOSSEN DEVICE
The Luftwaffe tried to surmount the problem of the
weapon being able to fire only a single round by
mounting it in groups of as many as 49, to be set off
in ripple salvoes. Recoilless guns were mounted to
fire both forwards and upwards; pilots of single-seater
aircraft found aiming the latter to be somewhat problematic,
and so a trigger unit which incorporated a
light source and a photoelectric cell, the so-called
'Zossen' device, was developed. Tt was tested successfully
in 1944, but very few were ever fitted to aircraft.
An even more complicated automatic trigger
was developed for a downward-firing recoilless rifle
for use against tanks, detecting the tank's magnetic
field and using that to trigger the gun when the aircraft
was directly overhead.
Perhaps the most ambitious plan ever involving
gun armament for aircraft was put forward early in
1939. The Gerät 104 was a 35cm-calibre recoilless
gun which fired a 635kg (14001b) armour-piercing
shell (the cartridge case weighed the same, and thus
acted as the counter-shot itself). It was intended for
use against ships of the Royal Navy lying at anchor in
Scapa Flow (a place of special importance to the
Germans, of course, not just because it dominated the
northern approaches, but also as the site of the scuttling
of the High Seas Fleet in 1919), but in the event,
the plan came to nothing. However, later an even bigger
weapon, the 54cm 'Munchausen' cannon, was
proposed, and it seems that a prototype was constructed
and mounted beneath a Junkers Ju 87 Stuka
dive-bomber. Not entirely unsurprisingly, the effect of
firing such a weapon, recoilless or not, upon a relatively
light aircraft was unpredictable to say the least
and the project was cancelled.
Another, and simpler, solution to the recoil problem
was to substitute rockets - which have no recoil
- for guns, and almost from the outset, this proved to
be successful. Initially, the weapon used was a cutdown
version of the Army's 21cm Nebelwerfer 42
rocket launcher, mounted in various ways, which was
eventually superseded by the 5.5cm R4M rocket. The
21cm rockets were first fitted in pairs to Fw 190s;
they could be jettisoned after use, and most pilots
AIR-TO-AIR WEAPONS
adopted this procedure, for they robbed the aircraft of
about 50km/h (30mph). They were used against
bomber formations, and also as air-to-ground
weapons. Twin-engine fighters such as the Bf 110 and
Me 410 were fitted with larger batteries. They were
not only employed as forward-firing weapons; a few
Ju 88s and He 177s were modified to carry up to 24
launchers within the fuselage, angled to fire upwards,
while some Fw 190s carried a single rearwards-firing
tube. The rocket itself, the 21cm Wurfgranate
(Spreng), was a powerful weapon, with a 10.2kg
(22.41b) warhead and an intial velocity of 320m/s
(1050fps). As an artillery bombardment rocket it had
a range of about 8000m (8750 yards); in the air it was
reckoned to be effective out to 800-1200m
(875-1300 yards).
THE R4M
The R4M was more effective: with its much smaller
profile it produced less drag, and more could be carried.
The usual load for an Me 262 was 24, in a rack
under each wing outboard of the engines, but that
could be doubled when necessary by adding another
pair of racks. The racks were mounted at an upwards
inclination of 8 degrees, and the missiles were fired
serially, at a fraction of a second's interval (a 'ripple
salvo'), at a range of around 600m (660yds). The
R4M was simplicity itself: a stick of diglycol solid
fuel which, being nitrocellulose based, burned at a
predictable rate based on the surface area exposed to
the atmosphere, with a contact-fuzed warhead and
spring-loaded stabilising fins, which deployed as soon
as it left the launch tube (originally of metal, but later
of carboard). Measuring 82cm (32.2in) long and
5.5cm (2.16in) in diameter, it was adapted for a variety
of purposes but was mainly employed against aircraft
and tanks. It was virtually identical to the British
3in (7.62cm) rocket which preceded it into service by
some years. 'Föhn', its putative successor, was a
somewhat larger but essentially similar device, originally
designed as an anti-aircraft weapon. With a
diameter of 7.3cm (2.8in), it had a conventional warhead
containing 250g (8.8oz) of TNT/RDX (the
R4M's anti-aircraft warhead, the PB-3, was a shapedcharge,
with 400g (14oz) of Hexogen). Few, if any,
were used operationally.
One of the advantages of the R4M was that since
the rocket had the same short-range ballistics as the
30mm cannon shell, the existing cockpit gunsight
could be employed, but unfortunately, that was saying
very little, for it was not an easy task to take accurate

AIR-TO-AIR WEAPONS
aim on a target which was taking evasive action from
a fast-flying aircraft whose flight characteristics
caused it to snake at high speed. The answer, of
course, was to provide a guidance system to control
the missile in flight.
AIR-TO-AIR MISSILES
From as early as 1939, the Henschel company - a
newcomer to aviation, but with a very solid background
in heavy engineering - had maintained a team
whose task was to study the remote control of
unmanned aircraft. In January 1940, Herbert Wagner
arrived to head the team, with a brief from the RLM
to concentrate on air-to-surf ace missiles (ASMs). He
was successful, as we shall discover, and in 1943 the
company proposed a version of the Hs 293 ASM he
developed as an air-to-air missile (AAM). Like most
of the ASMs, the Hs 293H was a blast weapon, to be
guided into a bomber formation and exploded there,
instead of being aimed at an individual aircraft, and
had a 295kg (6501b) warhead. One version of it was
to have had a television camera in its nose, the picture
it transmitted to the controller allowing him a clear
view at ranges of up to about 4km (2.5 miles), but the
apparatus proved very unreliable, and the idea, also
tried out on the ASM itself, was shelved. Control was
line-of-sight from the launch aircraft, the operator
using a joystick to initiate radio signals which in turn
actuated control surfaces on the missile itself.
This system was to be used in all the German guided
missiles, and will be explained more fully below,
in the context of the surface-to-air missiles for which
it was originally developed. The missile had both
command and proximity fuzes as well as a barometric
fuze to ensure that it would self-destruct before it
hit the ground. It was powered by a specially designed
Schmidding rocket which used M-Stoff (methanol)
and A-Stoff (oxygen), the latter being, unusually, in
gaseous form, to produce 610kg (13401b) of static
thrust for 11 seconds. The Hs 293 was too big and
clumsy for the anti-aircraft role, and it comes as no
surprise to discover that after some initial enthusiasm,
the RLM went cold on the idea. By then, however,
Henschel had begun work on the 'Schmetterling' surface-to-air
missile (SAM; see Chapter Eight), and had
proposed a version for use in the AAM role.
THE HENSCHEL Hs117H
The Hs 117H, as the variant was known, was very little
different from the basic 'Schmetterling', save that
it required no external booster rockets, but it had a
significantly larger warhead, containing 100kg
(2201b) of explosive. It employed the same guidance
system as the Hs 293H. The intended range of the Hs
I17H was 6-10km (3.7-6.2 miles), at up to 5000m
(16,500ft) above the 'parent' aircraft, which was a
considerable improvement over the earlier missile. It
was still in development at the war's end, having survived
the axe which descended on so many development
projects in January 1945, it is suggested, simply
because it had so much in common with the ASM
from which it was descended.
Henschel also developed a missile specifically
intended for use in the air-to-air role, the Hs 298, considerably
smaller than either of the others and with
reduced range. Like them, it had swept-back wings
and a tailplane with short fins at its extremities, and
control was by means of solenoid-operated 'Wagner
bars' responding to radio signals. The motor was a
solid-fuel two-stage Schmidding 109-543 which gave
150kg (3301b) of thrust for five-and-a-half seconds
followed by 50kg (HOlb) of thrust for 20 seconds.
The first experimental Hs 298 was fired in May 1944,
and altogether some 300 were produced and expended
in trials. With a warhead containing either 25kg
(551b) or 48kg (1061b) of explosive, detonated on
command or by a proximity fuze, it had a range of up
to 2500m (2735 yards), travelled at either 940km/h
(585mph) or 680km/h (425mph), and was designed to
be deployed aboard piston-engined aircraft such as
Do 217s, Fw 190s and Ju 88s. Development ceased in
favour of the Ruhrstahl X-4 in January 1945.
THE RUHRSTAHL X-4
Ruhrstahl AG was, as its name suggests, a steelmaker.
In 1940 it was ordered to collaborate with Dr Max
Kramer of the DVL to develop a series of bombs and
missiles using the spoiler control method the latter
had demonstrated two years earlier. This collaboration
was to result in three very interesting missiles:
the so-called 'Fritz-X' guided glider bomb; the X-7
'Rottkappchen' ('Red Riding Hood') anti-tank missile;
and the X-4 air-to-air missile. Development of
the X-4 began in 1943 in parallel with Henschel's Hs
298. These two missiles had very similar specifications,
though it appears that the X-4 was designed
from the start to operate with jet aircraft, and thus
flew at higher speeds. The primary difference
between the X-4 and other missiles was that it was
equipped not with wings and a tailplane, but with two
sets of four fins, one set swept back at an acute angle,
with parallel chord width roughly halfway back from

Above: The Ruhrstahl X-4 was the most sophisticated of
all the air-to-air missiles produced during World War II. It
had an ingenious wire-based guidance system.
the nose; the other, offset by 45 degrees and carrying
the moveable spoilers, at the tail. Secondarily, it was
designed from the outset to be guided by wire, rather
than radio signals - as it was planned to switch over
to control by wire for all missiles since radio signals
were simply too easy to jam - the necessary differentiation
being obtained by switching the polarity of the
signal to activate the pitch controls, and by varying its
strength to activate the yaw controls. This system
used the Düsseldorf/Detmold (FuG 510/238) transmitter-receiver
pair, which were analogous to the
Kehl/Strassburg radio transmitter and receiver. It was
originally developed for use with the glide bomb, as
we shall see in due course.
As we noted when discussing the surface-to-surface
missiles, a cylindrical body in flight has a tendency to
roll. The small fin-tip vanes necessary to correct the
tendency in the X-4 would have interfered with
Kramer's control spoilers, so instead of trying to correct
it, the X-4's designers encouraged and controlled
it to a rate of about one revolution per second by fitting
offset trim tabs to the main fins. This, it was
believed, had the subsidiary effect of nullifying manufacturing
inaccuracies causing imbalance (which
would have thrown the missile off its line) just as the
rifling in a gun's barrel does. Because of the spin,
though, it was necessary to fit a gyroscopic unit which
switched the control signals between the spoilers on
the rear fins so that those which controlled pitch while
they were within 45 degrees of the horizontal changed
over to controlling yaw as they came within 45
degrees of the vertical, and vice-versa. The 5.5km-
(3.5 mile-) long wires carrying the positive and return
components of the electrical signal were paid out
from bobbins in streamlined pods on the tips of two
of the main fins. It mattered not at all that the control
wires became twisted as the missile spun, for it made
a maximum of perhaps 24 revolutions in the entire
course of its flight. It was planned to use the liquidfuelled
BMW 109-548 rocket to power the missile,
and in order to counteract any tendency the spin (and
any violent manoeuvres in flight) had to disrupt fuel
flow, the tanks which contained the R-Stoff and SV-
Stoff were spirally wound concentrically within the
double-tapering cylindrical form of the missile's
body. They contained free-moving pistons - leather in
the R-Stoff tank, aluminium in the acidic oxidizer -
driven by compressed air. The motor, producing
140kg (310Ib) of thrust reducing to 30kg (661b) by the
end of its 17-second burn time, was only ever used in
some of the test launches, Schmidding 109-603 diglycol
solid-fuel motors being substituted.
The first test firing of the missile from an aircraft
(an Fw 190) took place on 11 August 1944, and by
that time a total of 224 prototypes had been produced.
In all, about 1000 airframes were then produced for
operational use between August and December 1944,
but there were delays in engine production. Then, just
as the problems were ironed out, the BMW plant
which was manufacturing the 109-548 was badly
damaged in an air raid, and the motors which had
been belatedly produced were destroyed. This was the
final nail in the X-4's coffin and the missile never saw
operational service as a result.

CHAPTER SEVEN
Air-to-Surface
Missiles
Hitting a target on the ground with a bomb dropped from an aircraft was never easy;
as soon as effective anti-aircraft artillery and fighter aircraft were added to the
equation, it became very costly, too, particularly in human lives. By the end of the
twentieth century, stand-off bombing using remote guidance was to become
commonplace, but at the time of World War II this was pure fantasy - until German
During the Spanish Civil War of 1936-1939, the
Luftwaffe discovered that the only really effective
way to deliver bombs on to a point target was in
a near-vertical dive. This procedure they repeated in
1939 in Poland and in 1940 in the Low Countries and
France. Over Britain, later in the year, the Luftwaffe
came across the basic flaw in this principle: dive
bombers were uncomfortably vulnerable to effective
Above: The Henschel Hs 294 guided aerial torpedo's tail
and wings were designed to break off on hitting the water.
Left: An early air-to-surface missile was the Blohm & Voss
Bv 143, mounted here on a Heinkel He 111H.
scientists took up the task.
fighter aircraft and concentrated anti-aircraft artillery.
As an alternative, there was always area bombing
from high altitude, but it was very wasteful and of little
use against isolated high-value targets. Warships at
sea were particularly difficult to hit, and the Luftwaffe
frequently found itself mounting costly raids on
important maritime targets which achieved little or
nothing. Quite early on, thoughts turned to the development
of a bomb which could be guided in flight.
THE RUHRSTAHL X-1
Ruhrstahl's X-4 air-to-air missile showed promise,
but it never lived up to it. Much more useful was the
guided bomb they produced as the X-1. It had a

AIR-TO-SURFACE MISSILES
plethora of names: the RLM called it the PC 1400X;
the Luftwaffe called it the 'Fritz-X'; and it has also
been referred to as the FX 1400 and simply as the FX.
However, its success was shortlived, despite having
been designed with cheapness and simplicity in mind.
It had as its starting point the Luftwaffe's standard
1400kg (30801b) bomb, either the cast-steel thickcased
SD (Sprengbombe Dickwandig) 1400 known as
'Fritz', or the forged-steel armour-piercing variant,
the PC (Panzersprengbombe Cylindrisch) 1400. The
original bomb, manufactured by Rheinmetall-Borsig,
of perfectly conventional shape, was a plain cylinder
with a rounded nose coming to a blunt point and a
conical tail with four sheet-metal fins partially
shrouded by a strengthening ring at the extremity.
Ruhrstahl modified the overall form somewhat for its
guided bomb, leaving the last part of the cylinder
intact but introducing an oversize ogival form to the
first two-thirds of its length.
In order to maximise its aerodynamic performance,
they gave it four relatively large fins, located
forward of the mid-point of the bomb's length, with
square leading edges and a pronounced sweep to the
trailing edges. These main fins were mounted asymmetrically,
as if they formed the diagonals of a rectangle
with sides in the ratio one-and-a-half to one.
The 12-sided framework which replaced the simple
fin-and-shroud empennage maintained that same
basic rectangular form, but with the corners cut off.
Within it were four smaller fins, set vertically and
horizontally and containing the spoilers themselves,
simple tabs which were actuated by electro-magnets
and which caused disturbance within the airflow over
the appropriate surface of the fin when they were
deployed. Deployment in turn caused the whole bomb
to alter course or angle of descent by swinging it
around the axis formed by the straight leading edge of
the main fins.
RADIO GUIDED
Guidance was by means of a radio link using the
Kehl/Strassburg system (but later, the wire-link control
system was adapted for use with the X-l too),
while flares, or battery-powered lamps on the tail for
use at night, helped the operator to keep track of the
missile in flight. It was a simple, fairly ingenious system,
and it worked well enough, so long as the bomb
was dropped from sufficient height. Released at the
minimum altitude of 4000m (13,125ft) it had a range
of up to 4.5km (2.8 miles); dropped from the maximum
height any of its carrying aircraft could attain of
92
8000m (26,250ft), the range was up to 9km (5.6
miles). It was capable of piercing 130mm (5.125 in) of
armour plate when dropped from 6000m (19,700ft).
Though it is often referred to as a glider bomb, that is
not actually the case. Its forward speed was that
imparted by the launching aircraft, and it certainly did
not 'fly' in any accepted sense. Its only major vector
was downwards, and all the spoilers could do was
modify its path to a small degree. That was often
enough to make the difference between success and
failure, as we shall see later when we look at operational
deployment of the ASMs. A total of 1386 X-ls
were produced between April 1943 and December
1944, when manufacturing ceased, and this was far
short of the planned figure of 750 per month. Less
than half of them - a total of 602 - were expended, in
testing, training and operations.
THE RUHRSTAHL X-1 IN ACTION
From 29 August 1943, III Gruppe/Kampfgeschwader
100 (HI/KG 100), equipped with Dornier 217K-2s
and operating out of Istres near Marseilles, was the
first unit to employ Ruhrstahl X-ls to attack Allied
shipping in the Mediterranean. Initially they were
unsuccessful, but within a fortnight they had scored
heavily and it soon became clear that the X-1 was a
very potent weapon indeed.
On 4 September, Italy abandoned the Axis and
reached a separate peace with the Allies, but there
were still no clear indications of which way the powerful
but until now seriously misused Italian Navy
would jump. On 9 September the Allies landed at
Salerno, and at 12 noon that day, reconnaissance
reported that the Italian Fleet was at sea, headed south
for Malta. Within two hours, 12 Do 217s of III
Gruppe, led by Major Bernhard Jope, each armed
with a single X-1, were in the air. They headed east at
low altitude, then, climbing as they neared the coast
of Sardinia, made out the shapes of three battleships
with an escort of six cruisers and eight destroyers,
Jope led his formation to 6500m (7108 yards) and
turned towards the ships, which were now zig-zagging
wildly and firing every one of their anti-aircraft
guns. The first missile, launched by Oberleutnant
Heinrich Schmelz (who was to be awarded the
Knight's Cross, and later go on to command the
group), struck the 40,000-tonne (39,368-ton) battleship
Roma amidships at a terminal velocity of about
330 metres (1080 feet) per second, punching straight
through her bottom to explode beneath the ship. A
second hit her just forward of the bridge, where her

armoured deck slowed it down fractionally, so that it
exploded in the forward magazine beneath. She broke
in two and sank within 40 minutes, carrying 1255
men down with her, including the commanding admiral,
Bergamini. Her sister-ship the Italia was also hit
by a missile which passed through the deck and side
just forward of 'A' turret (ie, the most forward turret)
before exploding in the sea. She took in 800 tonnes
(787 tons) of water, but managed to make Malta,
though she played no further part in the war.
More successes followed. On 11 September, the
10,000 tonne (9842-ton) American cruiser USS
Savannah was disabled, as, two days later, was HMS
Uganda (8500 tonnes; 8365 tons). Better still was the
attack Jope himself carried out on the 33,000-tonne
(32,478-ton) British battleship HMS Warspite, which
was giving fire support off the Salerno beaches. The
missile hit the Warspite amidships, and penetrated six
decks before exploding against the bottom of the ship,
blowing a large hole in her. She took in a total of 5000
tonnes (4921 tons) of water, lost steam (and thus all
power, both to the ship herself and to all her systems),
and had to be taken in tow. She reached Malta but was
out of action for the next 12 months. The British
AIR-TO-SURFACE MISSILES
Above: The Ruhrstahl X-1, also known as the Tritz-X', was
one of the least sophisticated air-to-surface weapons, but
one of the most successful. On 9 September 1943, two of
these guided bombs sank the Italian battleship Roma.
cruiser HMS Spartan and the destroyer HMS Janus
were also sunk by X-ls, and the American cruiser
USS Philadelphia was badly damaged.
THEHENSCHELHs293
The Ruhrstahl X-1 development programme began at
around the same time that Wagner's team at Henschel
began work on the Hs 293. Surprisingly, development
took longer, but it proved to be much simpler to train
aircrew to 'fly' the bomb than the missile, and the two
were eventually deployed together. Initially, the RLM
had tried to persuade Henschel to produce a missile
which levelled out just above the water some distance
before reaching the target, and another which would
actually submerge and act like a conventional torpedo,
but the company refused on the grounds that such
a course would be too ambitious, since there was no
experience on which to draw. Instead, it put forward
the concept of a straightforward guided glider bomb,

AIR-TO-SURFACE MISSILES
FOCKE-WULF Fw 200C-6
Type: Long-range maritime
reconnaissance bomber
Length: 23.85m (76.96ft)
Span: 32.84m (107.79ft)
unpowered but with aerodynamic properties, and the
RLM agreed. The first experimental version, with no
warhead, was tested in the spring of 1940, and by the
end of the year a variant with a rocket motor, which
allowed launch at 400m (1315ft) instead of the
1000m (3280ft) previously required, had been flown
successfully, and plans for a production version of the
latter were going ahead.
10 SECONDS OF THRUST
The Hs 293A-1 was built up from the nose and body
sections of an SC (Sprengbombe Cylindrisch) 500
thin-walled bomb, with an elongated rear section
tapering in the vertical plane, which extended above
and below the body unequally to form small dorsal
and larger ventral fins, carrying the guidance system.
Short symmetrical wings with conventional ailerons
were mounted where the bomb and tail section joined,
and a tailplane with an equally conventional elevator
was mounted just above their plane, where it would
operate in clear air. The ailerons were actuated by
electromagnets; the elevator by an electric motor and
worm screw. The rocket motor - a liquid-propellant
Walter 109-507B, using T-Stoff and Z-Stoff held in
pressurised tanks - was underslung beneath the fuselage
in a pod; it gave only 600kg (13001b) of thrust for
10 seconds, but that was enough to propel the missile
well ahead of the aircraft to a point where the bomb
aimer could see it. This had been a recurring problem
with the X-l, and one which could only be solved by
the pilot of the launch aircraft throttling back and
lowering his flaps until the aircraft almost stalled,
which made him very vulnerable indeed.
The flight profile of the Hs 293 was quite different
from that of the X-l. It was normally released at
between 400m (1315ft) and 2000m (6560ft), and
94
Max take-off weight: 22,700kg (50,044lb)
Max speed: 360km/h (224mph) at 4700m (15,420ft)
Range: 3560km (2211 miles)
Payload: 2 x Hs 293A guided missiles
Above: One of the German aircraft equipped to employ the
Hs 293 rocket-propelled guided bomb was the long-range
Focke-Wulf Fw 200 'Condor'. Two missiles could be
carried, under the outboard engine nacelles.
between 3.5km (2.2 miles) and 18km (11 miles) short
of the target. The terminal velocity varied between
435km/h (270mph) and 900km/h (560mph) depending
on the altitude from which it had been released.
Control, as always, was by joystick and radio link, on
the Kehl/Strassburg system, but wire linkage was
soon proposed and implemented, this time using a
duplex bobbin system, with the wire being paid out
from aircraft and missile simultaneously, giving a
maximum range of 30km (18.7 miles). As with the X-
1, flares in the tail - which were exchanged for small
battery-powered lamps for night operations - allowed
the bomb-aimer to keep track of the missile in flight.
A version of the basic weapon, with an extended
nose to contain a television camera, was developed as
the Hs 293D. The television equipment was developed
by Fernseh GmbH in collaboration with the
Reichspost-Forschungsanstalt. It was a vertical rasterscan
224-line system operating at 50Hz. Under ideal
(laboratory) conditions, with its inventors to operate
it, the system worked adequately enough, but under
operational conditions it was much less successful
and was finally abandoned. Such technology was not
yet fully understood, and it was to be many years
before it was perfected in weapons such as the American
AGM-65 'Maverick' and the Anglo-French
'Martel'of the 1980s.
Other Hs 293 variants included the Hs 293H,
which was discussed above in the context of air-to-air
missiles, and the delta-winged, tailess (and stillborn)
Hs 293F. It is unclear how many Hs 293s of all types

DORNIER Do 217E-5
Type: Four-seat anti-shipping bomber
Length: 18.20m (60.00ft)
Span: 19.00m (62.33ft)
Max take-off weight: 16,465kg (36,299lb)
Max speed: 515km/h (320mph) at 5200m
(17,060ft)
were manufactured, but educated guesses put the
number at perhaps 1500, many of which were
expended in the long testing and training programme.
THE HS 293 IN ACTION
II Gruppe of Kampfgeschwader 100, flying Hs 293 Aequipped
Do 217E-5s out of Cognac under Hauptmann
Heinz Molinus, was the first unit to go into
Range: 2300km (1429 miles)
Payload: 2 x Hs 293A guided missiles
AIR-TO-SURFACE MISSILES
Above: Somewhat more successful than the Fw 200 was
the Dornier Do 217E-5, which also carried two Hs 293As
under its wings. It was one of these aircraft, of I I/KG 100,
which scored the first success with the new weapon,
Below: The bomb-aimer needed to keep the Hs 293 in
sight all the way to the target, and for this purpose a
multi-tube flare unit was attached to the bomb's tail.

AIR-TO-SURFACE MISSILES
Above: The bomb-aimer controlled the Hs 293 using a
two-axis joystick which transmitted signals either by radio
or over wires. This installation is in an He 111H-12.
action armed with guided air-to-surface missiles, on
25 August 1943, against warships hunting German
submarines in the Bay of Biscay. The first-ever kill
with a guided missile came on 27 August, when one
scored a direct hit on the 1270-tonne (1250-ton) sloop
(ie, corvette) HMS Egret, detonating the ammunition
96
in her after magazine and blowing her to pieces with
the loss of 222 lives. In fact, II/KG100 later moved to
Tstres, near Marseilles, and II/KG40, equipped with
He 177A-5s, replaced it on the Atlantic coast. Besides
the Egret, Hs 293s accounted for five destroyers and a
number of merchant ships before the Allies found a
way to combat them using a set of defensive tactics
which included jamming the radio control signals and
targeting the launch aircraft during the vulnerable
control phase, when they had to fly straight and level

at reduced speed. These defensive tactics made the
missions very costly. On 23 November, II/KG40 lost
half its entire strength while attacking a well-protected
convoy off the Algerian coast. Hs 293s were last
used in action, with some success, against Red Army
forces crossing the River Oder in April 1945, when
they went into action with 'Mistel' (qv) piggyback
hybrid aircraft.
THE BLOHM & VOSS ASMS
Blohm & Voss reacted to the RLM's requirement for
a sea-skimming missile with a proposal for a guided
glider bomb. This incorporated a rocket motor which
was only ignited by tripping a 2m- (6.5ft-) long lever
hanging from its underside when the bomb came to
the end of its descent. It was an ingenious solution,
but proved to be unworkable. The length of time
available to initiate the rocket motor was just insufficient,
and the prototypes simply ploughed into the
sea. Rather better conceived was the Bv 246
'Hagelkorn' ('Hailstone'), which was a pure glider
and was intended specifically to attack radio stations
transmitting navigational signals to RAF bombers by
homing in on their very signals. The Bv 246 was a
simple aerodynamic shape with a cruciform empennage
incorporating a vertical control surface, and high
AIR-TO-SURFACE MISSILES
aspect-ratio wings designed to give it a shallow glide
angle (1:25, or barely 4 degrees) and thus a long range
after launch. Released at 10,500m (34,450ft), it had a
range of 210km (130 miles). The original proposal
was made in 1942, but there was little official interest
despite the fact that the RAF had already begun to use
radio as a navigational aid. It was December 1943
before 'Hagelkorn' was ordered into production and it
was cancelled two months later in the February 1944
austerity drive, by which time hundreds had been
built. These missiles were gradually expended in a
protracted low-priority test programme which lasted
until January 1945. With an all-up weight of 730kg
(16001b), of which 435kg (9601b) was warhead, it was
light enough to be deployed by an Fw 190.
FLYING TORPEDOES
The RLM did not give up its search for an air-to-subsurface
weapon, and Henschel responded eventually
with a variety of designs for what we may regard as
guided air-launched torpedoes. The simplest of these
Below: The Blohm & Voss Bv 143 was a rocket-assisted
glider bomb, the powerplant of which was ignited only
when the projectile had come within 2m (6.5ft) of the
surface of the sea.

AIR-TO-SURFACE MISSILES
Above: The Dornier Do 217 was the aircraft of choice for
the deployment of the Henschel Hs 294 anti-ship missile.
Perhaps 1450 of these sophisticated guided missiles were
ordered but few were completed.
98
Below: This sequence shows a launch of an Hs 294 which
went disastrously wrong. Having disengaged from the
parent Do 217 aircraft, the missile then collided with the
bomber, slicing off a tail fin.

HENSCHEL Hs 294
Type: Rocket-propelled anti-ship missile
Length: 6.12m (20.08ft)
Span: 4.025m (13.21ft)
Total weight: 2170kg (4784lb)
was a version of the Hs 293, and from that, in 1943,
sprang the larger and more powerful Hs 294, intended
to be used to attack armoured ships. Two versions
were produced in prototype form, one with radio
guidance, the other with a wire command link.
The Hs 294 was essentially of the same form as the
air-to-surface missile, with the addition of a long,
tapered nose cone and a second rocket unit. It was to
be flown into the sea at a shallow angle (optimum 22
degrees); the wings and the rear fuselage were mounted
so that they would break away on hitting the water,
and the warhead, with its 656kg (14451b) explosive
charge, would then be free to travel in a parabolic
path, induced by the form of its upper surface, for up
to 45m (150ft), self-destructing if it had not found its
target. It is believed that a total of around 1450 were
ordered, but few were produced.
The Hs 294 was followed by a rather more ambitious
project known as the GT 1200, which certainly
did not get past the prototype stage. GT 1200 was to
have been an unpowered glider, with the guidance
Max speed: 860km/h (534mph)
Range: 4-14km (2.5-8.7 miles)
Payload: 656kg (1445lb) of explosives
AIR-TO-SURFACE MISSILES
Above: The Hs 294 was intended to enter the water
cleanly some way from its target and strike it below the
waterline, where it was at its most vulnerable.
package of the Hs 293, but without a rocket motor to
assist its launch. Instead, the rocket motor, a standard
Schmidding solid-fuel unit, was to have been used
only during the last phase of its deployment, underwater,
when, shorn of its wings and 'fuselage' extension,
it became an otherwise conventional torpedo,
steered by small rudders on its cruciform rear-mounted
fins. There is no indication of how the missile was
to have been guided during its run through the water.
Hensehel's last foray into the field of air-launched
submarine weapons was to have been a supersonic
missile known as the 'Zitterrochen' (Torpedo Fish'),
its triangular planform wings incorporating 'Wagner
bars' - simply spoilers moved to the wing trailing
edge - instead of ailerons. The project never got off
the ground, but the control system found its way into
the Hs 117 'Schmetterling' and the Hs 298.
99

CHAPTER EIGHT
Surface-to-Air
Missiles
In parallel with the programmes to develop air-to-air and air-to-surface missiles,
German scientists and engineers also strove to produce guided surface-to-air
missiles (SAMs). Work first began in 1941, but yet again, progress was overtaken by
events; the first usable missiles were due to go into service in mid-1945, but by then
the war was already over.
Finding ways to defeat the Allied bomber formations
which pounded the Reich preoccupied the
Luftwaffe and the RLM alike. As a result, a number
of teams were at work developing new weapons. Most
important amongst these were the more-or-less successful
jet and rocket-powered aircraft we have
already discussed. However, much energy and
resources went into developing surface-to-air missiles
(SAMs) too, amongst the most significant of which
Above: The Messerschmitt 'Enzian' was made largely of
plywood and flew at subsonic speeds.
Left: Like the 'Enzian', the 'Wasserfall' relied on blast
effects; its warhead was detonated by an artillery fuze.
were the Henschel Hs 117 'Schmetterling'
('Butterfly'), the Messerschmitt 'Enzian' ('Gentian'),
the Rheinmetall-Borsig 'Rheintochter' ('Rhine
Maiden'), and the BMW 'Wasserfall' ('Waterfall') -
all of which had a guidance system - and the BMW
Taifun' (Typhoon'), which was unguided.
THE HENSCHEL Hs 117 'SCHMETTERLING'
The earliest of the projects was for a subsonic shortto-medium-range
missile which was radio controlled
by an operator on the ground. Henschel first began
work on the project in 1941, alongside a number of
unguided flak rockets, and two years later was
ordered to develop it as the Hs 117. With stubby
swept-back wings and a cruciform tail, the Hs 117
1 m

SURFACE-TO-AIR MISSILES
'Schmetterling' was controlled like an aircraft, with
solenoid-operated 'Wagner bars' rather than conventional
ailerons on the trailing edges of the wings and
tailplane. It appeared somewhat unbalanced, having a
bifurcated nose, with the starboard cone elongated to
form a warhead extension and the port cone finishing
in a small airscrew driving a generator. Launch power
was supplied by a pair of external solid-fuel motors,
one above and one below the fuselage, which gave
1750kg (38501b) of boost for four seconds, accelerating
the missile to 1100km/h (680mph) before falling
away and igniting the sustaincr motor. The motor was
to have been either a BMW 109-558 or a Walter 109-
729, both of which used liquid fuel - R-Stoff or
Tonka', a composite self-igniting fuel, with SV-Stoff
(concentrated nitric acid) as an oxidizer in the former;
SV-Stoff and Br-Stoff (low-octane petrol), with an
alcohol igniter, in the latter.
LAUNCHING THE 'SCHMETTERLING'
At 4.3m (14ft) long and weighing a total of 420kg
(9251b) including the solid-fuel motors, the
'Schmetterling' was launched from a modified antiaircraft
gun mounting, azimuth and elevation being
approximately pre-set manually by the launch crew.
102
Once in flight, a flare in the tail was ignited, and the
controller observed its progress through a telescope,
correcting by radio using the Kehl/Strassburg system
codenamed Tarsival' (FuG203/230), which was also
widely used for other operator-guided missiles,
employing four separate radio frequencies, two for
the horizontal axis and two for the vertical. Control
was by a simple joystick. A fifth radio frequency was
used to detonate the 25kg (551b) warhead, which
relied on blast rather than fragmentation, on command,
though proximitiy and time delay fuzes were
also developed. The effective range was 16km (10
miles) and the ceiling was 1 1,000m (36,000ft). In
blind conditions it was hoped to employ the
Mannheim-Reise/'Rheingold' radar system, which
worked something like the Würzburg fighter control
system, one set tracking the target, the other the missile;
the operator would use the joystick as before, but
would now be observing dots on a cathode ray tube,
and trying to keep them superimposed. Later, it was
hoped, corrections would be applied automatically.
Below: The Henschel Hs 117 'Schmetterling' was the first
attempt by Germany to develop a surface-to-air missile; it
was for use against low- and medium-altitude intruders.

MENSCH EL Hs 117
Type: Rocket-propelled surface-to-air missile
Length: 4.29m (14ft)
Diameter: 350mm (13.77in)
Testing of the 'Schmetterling' began in May 1944,
and by September, 22 launches had been made, some
of them of a variant intended as an air-to-air missile,
the Hs 117H (qv). The success rate was good enough
that the missile was ordered into production in
December, with first deliveries - 150 units per month
- to take place in March 1945, rising to 3000 per
month by November. This was hopelessly optimistic,
of course, at a time when industrial output in
Germany was failing fast, and no missile was ever
produced for operational use.
THE MESSERSCHMITT 'ENZIAN'
Messerschmitt's proposal resembled an unmanned
version of the Me 163 'Komet', with the same stubby
body and wings and the twin ventral/dorsal tail fins. It
was considerably heavier than the 'Schmetterling' at
1800kg (39701b), had a 300kg (6601b) warhead, and
was designed to operate at up to 12,000m (41,000ft)
or out to a range of 24.5km (15.25 miles) at lower
levels. One most important feature of the 'Enzian'
was the fact that its airframe was to be constructed of
moulded plywood, a material Germany had in abundance,
and this was almost - but not quite - enough to
give it sufficient official approval points to actually
see it into production, especially since it used technology
which was well understood.
The 'Enzian', originally the Flak Rakete l, was
designed from June 1943 by a team led by Hermann
Wurster at Messerschmitt's R&D headquarters at
Oberammergau, with prototypes to be produced at
Augsburg and serial airframe manufacture to be carried
out at Holzbau Kissing AG, in nearby Sonthofen.
Launch weight: 445kg (981 Ib)
Max range: 32km (20 miles}
Warhead: 25kg (55lb) of high explosive
SURFACE-TO-AIR MISSILES
Above: The Henschel Hs 117 'Schmetterling' surface-toair
missile. The Hs 117 was also produced in an air-to-air
version which lacked the SAM's external boosters.
Like the 'Komet', it had a circular-section fuselage,
0.9m (3ft) in maximum diameter; it also had ventral
and dorsal fins and mid-mounted swept-back wings
with full-width elevons, which operated in unison or
independently and thus obviated the need for a rudder.
Launch power was provided by four Schmidding
109-533 diglycol-fuelled rockets, the same as that
employed for the 'Schmetterling', which gave a combined
thrust of 7000kg (15,40015) for four seconds
and were then jettisoned. The launch platform consisted
of 6.8m (22.25ft) rails on a modified 8.8cm
anti-aircraft gun mounting, which could of course be
trained in azimuth and elevation. The sustainer rocket
was to have been a Walter R1-210B, using SV-Stoff
and Br-Stoff as its fuel, delivered to the combustion
chamber by a pair of steam-driven turbo-pumps as
employed in the A4. About 15 of these motors are
thought to have been produced, and they were used to
test the prototype missiles, but for the production version
a simplified motor was designed by Drs Konrad
and Beck of the Deutsches Versuchsanstalt für
Kraftfahrzeug- und Fahrzeugmotoren (DVK - the
German Aviation Propulsion Experimental
Establishment), which used S-Stoff and Visol delivered
by compressed air, and in its final form gave the
slightly higher performance figures of 2500kg
(55101b) of thrust falling to 1500kg (33001b) by the
end of its 56-second burn time. The reducing thrust
ensured that the missile did not exceed its maximum
03

SURFACE-TO-AIR MISSILES
Mach number and become unstable. Guidance was
exactly the same as for the 'Schmetterling' and the
same sort of proximity fuze was to have been used.
Perhaps 60 'Enzian' missiles were constructed, of
which 38 were tested, beginning in April 1944. The
first examples fared badly because the designers had
not grasped the importance of aligning the missile's
axial centre of gravity and thrust lines, but that was
cured, and later tests proved successful. The 'Enzian'
fell foul of the general deterioration in manufacturing
capacity, and as there was concern at RLM that it was
detracting from the production of Me 163s and Me
262s, in January 1945 the project was axed.
THE RHEINMETALL-BORSIG MISSILES
Although successful with its unguided 'Rheinbote'
bombardment missiles, Rheinmetall-Borsig achieved
less with its surface-to-air missiles. The company's
first foray into the field was a winged missile called
the 'Hecht' ('Pike'), which seems to have been no
more than a design and concept-proving exercise;
several are known to have been air-dropped, both in
powered and unpowered forms. Work on it stopped in
1941, when the 'Feuerlilie' project was initiated; it
MESSERSCHMITT 'ENZIAN'
Type: Rocket-propelled surface-to-air missile
Length: 2.4m (7.875ft)
Diameter: 0.88m (2.9ft)
104
seems that this, too, was to have been purely a
research programme, but the RLM insisted that it be
adaptable to use as an anti-aircraft rocket, should that
prove necessary. Even though there is no evidence
that that step was taken, and the missile was unguided,
we may include it here in passing.
The 'Firelily' was to have a streamlined cylindrical
fuselage with rear-mounted swept-back wings terminating
in small symmetrical fins. It was to have been
produced in a number of versions of different fuselage
diameter, the most important of which were the
F25 and the F55, and was to have been propelled by
solid-fuel rockets which the company already had in
production as take-off assistance units (RATO) for
gliders and heavily-loaded transport aircraft, though
there was also a plan to produce a supersonic version
of the 55cm missile, with simple fins in place of the
wing assembly, to be powered by a Konrad-designed
liquid-fuel rocket. The 'Firelily' project continued
Below: In looks, 'Enzian' resembled the Messerschmitt
Me 163 'Komet' rocket plane. Like all liquid-fuelled
rockets, most of the internal space of the 'Enzian'was
taken up with fuel tanks.
Launch weight: 1800kg (3970lb)
Max range: 24.5km (15.25 miles)
Warhead: 300kg (660lb) of explosives

until early 1945, but it seems clear that no attempt
was ever made to utilise the missiles as weapons.
Several F25s were manufactured and were tested at
Peenemunde-West and at the company's own proving
grounds at Leba, but certainly no operational variant
was ever produced. Perhaps six F55s were produced;
one was tested successfully at Leba, and two were
sent to Peenemünde, where the one went out of control
when launched.
The 'Rhine Maiden' was an entirely different matter.
It was conceived from the outset as an anti-aircraft
missile. It was an ambitious design incorporating two
stages: the cylindrical first stage housed nothing but
solid-fuel booster rockets, and had four fixed, sweptback
fins with bracing struts between them, which
acted simply as stabilisers, being jettisoned on burnout;
the second stage, also cylindrical, tapered to a
point at the nose and slightly at the tail, and had six
fixed fins mounted about two-thirds the way back
from' the nose, and four small rounded steering surfaces
- canards, in effect - at the nose itself, which
were actuated by servos to guide the rocket in flight.
Unusually, the warhead was situated in the rear of the
rocket, behind the fins and motor unit, the six venturi
of which were positioned between the fins, angled
out, which also worked to help stabilise the missile in
flight. 'Rheintochter F was intended to reach speeds
of almost 1300km/h (SOOmph), and carry a
100-150kg (220-3301b) warload to 40km (25 miles)
and 6000m (19,700ft). The missile had a lengthy
Above: Rheinmetall was better known for its artillery
pieces, but its 'Rheintochter' SAM was an ambitious
design intended to fly at up to 1300km/h (SOOmph).
development period. The contract was signed in
November 1942, but by late 1944 only a relatively
small number - perhaps 50 - had been launched, less
than half of which carried guidance equipment that
was essentially similar to that incorporated in
'Schmetterling' and 'Enzian' and in the more successful
guided glide bombs. At the year's end, the
project was abandoned, the missile never having
come close to reaching its design altitude.
It seems that the development team had known all
along that the RATO units would never produce the
required performance, and had planned to power the
production version of the missile, known as
'Rheintochter III', with a version of the same Konraddesigned
liquid-fuel rocket which was to go into the
supersonic 'Feuerlilie', though a version with a
much-enlarged solid-fuel rocket was also proposed.
This was, in fact, the only version of the
'Rheintochter IIP ever tested.
THE EMW'WASSERFALL
Although Wernher von Braun worked for the German
Army, and anti-aircraft defences were the responsibility
of the Luftwaffe, EMW was ordered to produce an
anti-aircraft guided missile. Most of the necessary
work had already been done in developing the A4,
105

Above: The 'Rheintochter' 1 on its launch ramp. Guidance
was provided by the small vanes at the nose, which were
controlled from the ground via radio signals.
and the chief difference between 'Wasserfall' - as the
surface-to-air missile was known - and the A4 was to
be in its propulsion plant. From the outset it was clear
that the operational requirements for the two rockets
were quite different. Whereas A4 could be fuelled as
and when required, in a more or less leisurely fashion,
and fired when it was ready, the SAM would be
required to be held at instant readiness, perhaps for
months, and this was simply not practical if a cryogenic
propellant like liquid oxygen was employed.
Instead, it would be fuelled by Salbei (90 per cent
nitric acid, 10 per cent sulphuric acid to inhibit corrosion)
and a type of Visol, the fuel - which ignited
spontaneously on being combined - being delivered
to the combustion chamber by pressurising the propellant
tanks with inert nitrogen, rather than by using
cumbersome high-pressure steam turbines. Because
the two components of the fuel reacted so violently,
pre-launch and launch-time safety procedures very
important, and there was an elaborate system of interlocks
involving metal membranes which would rupture
only in predetermined circumstances.
'WasserfaU' was about half the length of the A4, at
7.84m (25.7ft), and weighed 3500kg (77201b) all-up,
as opposed to 12,900kg (28,4401b), but it was still by
far the biggest of all the German surface-to-air
106
weapons, even though its warhead was smaller, at
235kg (5201b), than that of the 'Enzian'. It was very
similar in shape to the bigger missile, but unlike the
A4 it had four stabilising fins located about one third
the way back from the nose.
35 TEST LAUNCHES
'Wasserfair was designed to operate at greater range
and altitude than the other SAMs. Its 8000kg-
(17,6301b-) thrust engine burned for 40 seconds and
gave it a range of up to 50km (30 miles) and an altitude
of 20,000m (65,000ft), even though the latter
was far higher than any aircraft attained. Its guidance
system was manual and ground-based, with course
corrections transmitted to the rocket by radio signals,
but since it was launched vertically, it also carried the
A4's basic inertial guidance system, to point it in the
approximate direction of the target. It is difficult to
imagine visual tracking and control being at all effective
at anything like extreme range and altitude, and
given its high launch speed, guiding it manually at all,
whether through a sighting telescope or by superimposing
dots on an oscilloscope, generated by tracking
radars, must have presented problems. The first successful
launch occurred at Peenemiinde on 29
February 1944, and it is believed that about 35 test
launches were made in total. Series production was to
have been at the biggest underground factory of them
all, Bleichrode, but in the event even the factory itself
had not been built when the war ended in May 1945.

THE UNGUIDED 'TAIFUN'
By mid-1944, there were many in Germany who
advocated cancelling the offensive weapons development
programme completely in order to concentrate
on developing more effective defensive measures, but
of course Adolf Hitler was not one of them, and what
he said still went. The 'Aggregat' programme certainly
got priority at Peenemünde, and since the same
team was working on 'Wasserfall', that inevitably
meant that the latter lost out because resources were
not available. The A4 got into production, while
'Wasserfall' did not. Tn fact, there was not even a clear
consensus in favour of 'Wasserfall', or even general
acceptance of its desirability. Some at BMW even
advocated scrapping 'Wasserfall' (on the grounds that
it would never work successfully without an automatic
guidance system) and concentrating on a simpler,
unguided flak rocket.
A design for just such a missile was put forward by
the Range Officer at Peenemünde, an engineer named
Scheufein, and was - perhaps somewhat surprisingly,
considering all the other demands being put on that
establishment - ordered into development in
September 1944 as the Taifun' ('Typhoon'). The first
examples used solid-fuel motors, but it soon became
apparent that they would not reach the desired height
(the 'Rheintochter' development team was having the
same problem, we may recall), and liquid propellants
Salbei and Visol were used instead. They were stored
in concentric cylindrical tanks, which made up the
body of the missile, and forced into the combustion
SURFACE-TO-AIR MISSILES
chamber by nitrogen under pressure, a cunningly
designed valve ensuring that initially there was a fuelrich
mixture in the chamber which allowed pressure
there to build up slowly and evenly (relatively speaking
since the delay between triggering and firing was
one tenth of a second). This was to prove most effective,
and was to make 'Taifun' surprisingly accurate
even at high altitude, which meant that the warhead
could be fitted with a contact or graze fuze, and needed
to be no bigger than a conventional anti-aircraft
artillery shell of 0.5kg (1.lib).
Overall, the missile was 1.93m (6.3ft) long and
100mm (4in) in diameter. Tt weighed 21kg (461b)
before launch, and reached a height of 15,000m
(49,210ft) before falling back to earth, with a maximum
velocity of 3600km/h (2235mph). It went into
limited production at Peenemünde in January 1945,
and an estimated 600 were completed, along with a
small number of launchers (which were based, once
again, on the mounting of the 8.8cm FlaK 37). Unit
cost would have been very low and, at RM25, less
than a third of the price of a rifle. There is no clear
indication whether it was ever used operationally, and
no evidence to suggest that it ever brought down an
aircraft, though that is certainly possible, since to the
target's crew, it would have appeared that the aircraft
had been hit by conventional anti-aircraft fire.
Below: The 'Wasserfall' was essentially a scaled-down
A4 (V2) rocket; it weighed 3.5 tonnes (3.4 tons) and
reached an altitude of 20km (12.5 miles}.
107

CHAPTER NINE
Artillery
By the end of the nineteenth century, artillery pieces had already reached a very high
standard of sophistication, being able to hit small targets at ranges of 25km
(15.5 miles) and more. There was really very little left for gunmakers to do save to
make them bigger and yet bigger still, and that is just what the likes of Krupp, long
recognised as masters in the field, did.
Germany had some success with ultra-long-range
artillery during World War I, notably with the socalled
'Paris Gun'. The Imperial German Navy, which
constructed and manned them, called them the
'Kaiser Wilhelm Geschütz', and they were used sporadically
from March to July 1918 during the massive
and so nearly effective German counter-attack in
Picardy to bombard the French capital from the
region north of Soissons over 100km (60 miles) away.
They were 38cm (15in) naval guns, as mounted
aboard the battleships of the day, sleeved down to
21cm (8.25in) with liners whose rifling consisted of
Above: The K5 (E), a 28cm gun mounted on a railway car,
was perhaps the most successful of the 'superguns'.
Left: This 38cm gun, its barrel 45 calibres long, was
derived from a weapon designed for battleships.
deep grooves within which lugs on the shell located,
a method first adopted in the early days of the development
of the rifled gun in the 1840s. This same
method was to be employed in the very long-range
artillery pieces developed in Germany for use in
World War II - the K5 battlefield weapons and the
'strategic' K12, built to fire on England from the
French coast - though the shells of these guns were
rather more sophisticated. Heavily over-charged, they
projected their shell into the stratosphere where,
meeting little air resistance, it could extend its trajectory
considerably. The use of a far heavier charge than
the gun had ever been designed to employ soon
caused the barrel to wear out - it seems that 25cm
(lOin) of rifling was destroyed with every round fired,
and that a barrel's life was just 50 rounds in consequence
- and it then had to be rebored or relined. The
Paris Guns, with three mountings and seven barrels,
109

ARTILLERY
which were employed serially, fired just 303 rounds
towards Paris, slightly more than half of which (183)
actually landed within its boundaries, killing 256 and
wounding 620. These results made the entire project
highly cost-ineffective, except in propaganda terms.
Though these first-generation ultra-long-range
guns were to enjoy only limited success, they did,
albeit imperfectly, solve the problem of how to bombard
high-value area targets with relative impunity
from outside the range of counter-battery fire. In more
modern times they would be sickeningly vulnerable
to air attack, since they presented big targets, were
hard to conceal, and impossible to move at very short
notice, but in 1918, despite a huge campaign to locate
them, they were never found. By the time the Allies
overran the Forest of Crepy, where they were located,
there was no sign of them left save their concrete
emplacements. Another problem - and many said a
more pressing one - remained: how to subdue organised
defensive positions like the modern fortresses of
the Maginot Line, which ran down the French-German
border, in the shortest possible time. For this, a
Below: Krupp made two massive 80cm guns, 'Gustav' and
'Dora'; they fired a 7.1 -tonne (7-ton) anti-concrete shell
32km (20 miles} but required a crew of 2000.
80cm KANONE (EISENBAHN) 'SCHWERE GUSTAV
Calibre: 80.0cm (31.5in)
Barrel length: 28.957m (95.00ft)
Weight (overall): 1,350,000kg (2,976,190lb)
Weight of shell (anti-concrete): 7100kg (15,653lb)
Weight of shell (high explosive): 4800kg (10,582lb)
110
Range (HE): 47,100m (51,510 yards
task which was to be undertaken at shorter range, an
approach which can almost be characterised as 'brute
force and ignorance' was all that was necessary, and
the guns in question were no more than straightforward
developments of the siege guns which were
some of the first weapons deployed in 1914.
'BIG BERTHA'
In August of that year, the German Army advanced
through Belgium in order to execute the Schlicffen
Plan, sweeping through northern France to take Paris
from the northwest and thus avoid the hardened
defensive positions which dominated the approach
routes from Germany. For the most part, and exactly
as expected, they met little resistance, except from the
forts surrounding the vital city of Liege, and to subdue
these, they called up the big guns, the 42cm
(16.5in) siege howitzers. The operation took longer
than envisaged, but in the end ; Big Bertha' and her
sisters, as the British came to call the guns, prevailed.
They were not always to be so successful, however;
they were later taken to Verdun and used against the
fortress complex there to much less effect. These guns
were enormous, by any definition - after all, they
fired a shell which stood almost as high as a man, and
weighed in excess of a ton - and moving them was no

simple matter. In around 20 hours, they broke down
into 172 pieces, and could then be transported on 12
railway wagons. Not surprisingly (especially since it
was often necessary to construct railway lines first)
moving such monsters in and out of position was a
major operation, but there was no alternative, and the
sheer size of the guns was one of the most important
motives for the German Army's interest in much more
mobile rocketry. It had been a limiting factor in World
War I, and was to remain one in World War II.
Bertha was the daughter of Friedrich Alfred
Krupp, son of the founder of the company, and the
wife of Gustav von Bohlen und Halbach. 'Big Bertha'
had been manufactured by Krupp, and it was to the
Essen-based company that the Heereswaffenamt
(HWA - the German Army's weapons development
and procurement office) turned in the mid-1930s
when it realised that while the 'new' strategy of war,
the Blitzkrieg, once more placed the emphasis on
movement, there would still inevitably be fortresses
to subdue. In response to the HWA's request, Krupp's
engineers produced outline proposals for three guns,
of 70, 80 and 100cm calibre. The most realistic of
those was the 80cm gun, which would fire a projectile
weighing up to 7.11 tonnes (7 tons) to a range of
around 32km (20 miles). It would weigh around 1370
ARTILLERY
tonnes (1350 tons) and require a crew approaching
2000 strong. It would be mobile, but only in the loosest
possible sense, for it would take around three
weeks to dismantle it and the same to put it together
again, and would need twin railway tracks for the
whole of its journey, with an additional pair of tracks
for the cranes required for assembly and disassembly.
'GUSTAV AND'DORA'
Nothing more on the subject was heard from the
HWA, and Krupp's technicians went back to the more
realistic task of developing the K5 and K12. There the
matter may have rested, but in 1936, Hitler visited the
establishment and began asking about the possibility
of developing guns to defeat the Maginot Line. Gustav
Krupp told him of the 80cm gun project, and as
soon as the visit was concluded, well knowing
Hitler's weakness for the gargantuan, Krupp had his
staff draw up detailed plans. These were submitted to
the HWA early in 1937, and the response was an order
to construct three guns, work to start immediately and
to be completed by 1940.
In the event, the barrels proved very difficult to
manufacture, and Krupp missed the deadline by a
considerable margin. By the time they were ready to
proceed, the German Army had simply bypassed the
111

ARTILLERY
Above: The barrels of very large-calibre guns were
transported dismounted. This barrel was captured by
Allied forces at the war's end.
Maginot Line. With no suitable target immediately to
hand, work slowed down, and it was the end of the
year before the first barrel was completed, and 1941
before it was proofed. Only then was it worth setting
to work on building the very complicated carriage,
and that took the rest of the year. It was 1942 before
the first complete gun was transported to the firing
ranges at Rügenwald on the Baltic coast, assembled
and tested, in the presence of Hitler himself. All went
well and 'Gustav', as the gun had been christened, in
honour of the company's Chairman, was presented to
the nation with the company's compliments, to be followed
almost immediately by 'Dora', named after the
wife of the chief designer, Erich Muller.
THE BOMBARDMENT OF SEBASTOPOL
By 1942, the course of World War II had taken a drastic
turn following Hitler's declaration of war on the
Soviet Union. There may have been no worthwhile
1 12
targets for 'Gustav' in Western Europe, but there were
now plenty to the east. The gun was broken down into
its components, they were loaded aboard their specially
constructed railway flatcars, with the carriage
base trundling along independently, occupying twin
tracks, and the whole ensemble got underway for the
Crimea. 'Gustav' was set up some 16km (10 miles) to
the northeast of Sebastopol, which was still holding
out, where it fired 48 rounds in all (including one
which, most spectacularly, blew up an underground
magazine) and played a significant part in the fall of
the city, whereupon it was shipped back to Essen in
order for the barrel to be relined. 'Dora' took its place,
but it is doubtful whether it actually saw action, since
the Red Army soon counter-attacked and surrounded
the Germans, and by that time it had been safely evacuated.
There are no substantiated reports of either gun
having been used in anger again, though there are
reports of 'Gustav' having seen action at Leningrad
and 'Dora' having been sent to Warsaw to take part in
the bombardment after the uprising in 1944. At the
war's end, parts of 'Dora' were found near Leipzig,
parts of 'Gustav' in Bavaria, and components of the

third gun, which was never completed, in Essen. The
project proved to be a very expensive exercise in futility:
seven million Reichsmarks per gun, without the
cost of the special trains needed to transport them and
the manpower required both to manufacture and to
operate them. There were various schemes put forward
for improved versions on the original carriages.
These included one in 52cm calibre to fire a 1.42tonne
(1.4-ton) shell to a range of about 113km (70
miles); one to fire a 38cm sabotted sub-calibre shell to
over 145km (90 miles) and even to fire rocket-assisted
projectiles to something like 193km (120 miles);
and a smooth-bore version to fire a version of the finstabilised,
dart-like projectile called the Teenemunde
arrow shell' (Peenemünde Pfeilgeschoss\ developed
for the K5 gun (see below). None came to anything.
THE GERAT 041
The 'Gustav Gerät' guns were not the only fortresssmashers
constructed for the German Army. Rather
more satisfactory, and more practical, were the selfpropelled
60cm howitzers developed by Rheinmetall
ARTILLERY
as the Gerät 041, known unofficially as 'Karl', after
General Karl Becker, whose brainchild they were.
These were short-barrelled weapons, more like mortars
than howitzers, with a maximum range of 4.5km
(2.8 miles); they fired a 2.23-tonne (2.2-ton) shell
specially designed to destroy reinforced-concrete
structures such as blockhouses by burrowing into
them for 2.5m (8.2ft) before exploding their 240kg
(5291b) charge.
The complete ensemble weighed 124 tonnes (122
tons), and if the howitzers themselves were massive,
the carriages upon which they rode were hardly less
so at 11.3m (37ft) long, with full-length tracks with
eight, and later 11, small roadwheels, each one independently
sprung on a torsion bar. The vehicle could
be jacked down to allow its hull to rest on the ground,
thus avoiding the effects of recoil on the suspension.
The recoil system itself was duplex: the gun recoiled
Below: Rheinmetall constructed six 60cm self-propelled
mortars for the Wehrmacht. These 'fortress smashers' -
this is 'Thor' - were used all along the Eastern Front.

ARTILLERY
within a cradle, which in turn recoiled along the chassis,
controlled by hydro-pneumatic compensators.
The vehicles were powered by 44.5-litre motors,
although they were only expected to travel for short
distances under their own power. For longer journeys
they were loaded aboard specially built transporters
or on railway cars. Six were manufactured, together
with tracked, armoured ammunition carrier/loaders,
and were issued to 628 Heavy Artillery Battalion
(Motorised), which promptly named them 'Adam',
'Eve', 'Odin', 'Thor', 'Loki' and 'Ziu'. They first
went into action at the Siege of Brest-Litovsk in June
1941, and were also present at Lvov and Sebastopol
as well as elsewhere. In 1942, the Army asked for proposals
to increase their range, and Rheinmetall's
answer was to produce new barrels in 54cm calibre
which fired 1250kg (27551b) shells to a maximum
range of about 10km (6.2 miles). From then on, the
barrels seem to have been swapped to suit whatever
ordnance there was available. Two were seized by
American forces in Bavaria in 1945.
114
Above: The 60cm mortars fired a shell weighing 2.23
tonnes (2.2 tons), which was specially designed to drive
deep into a fortification before exploding.
THE K5 GUNS
Also considerably more practical than 'Gustav' and
'Dora' were the K5 guns in 28cm calibre, which fired
255kg (5651b) shells out to a range of close to 64km
(40 miles). A total of 28 of these were constructed
between 1936 and 1945, and all were used most effectively
in combat, the most famous probably being
'Anzio Annie', which was used to bombard the Anzio
beachhead, and is now on display at the US Army's
artillery proving grounds at Aberdeen, Maryland.
Like the Paris Guns, the K5 employed deeply incised
rifling - the 12 grooves were 7mm (0.25in) deep -
and each shell had very precisely machined curved
slots into which were inserted soft iron rails to form
splines, matching the pattern in the barrel exactly,
instead of the simple lugs or studs of the original.
These guns too were mounted on railway cars, though

unlike the 'Gustav Gerät', they were transportable
largely intact, and could thus be put into and out of
action much more quickly and easily. They were fully
practical weapons, and the smaller 24cm K3, built by
Rheinmetall, was perhaps better still, especially in its
improved form, the Krupp-developed K4.
However, that did not prevent the development of
projects to improve on these weapons. One of those
was to produce a rocket-assisted projectile (RAP),
which grew out of an attempt to develop a 15cm RAP
for an existing gun. This proved to be much more
practicable in the extra volume available. The shell
was in two parts, the head containing the solid propellant,
with a blast tube leading down to the base,
surrounded by a conventional high-explosive filling.
The propellant was ignited by a time fuze which detonated
19 seconds into the projectile's flight when it
was approaching the apogee of its trajectory and
boosted its velocity. The maximum range achieved on
test was 86.5km (53.7 miles), and it was calculated
that half the shells would land in an elongated target
area around 3500m (11,482ft) long and 200m (656ft)
wide, which was entirely acceptable given the nature
of the likely targets.
ARTILLERY
The RAP, an accepted part of the artilleryman's
arsenal only by the 1980s, was not the only new projectile
developed for the K5 gun. Scientists at Pennemünde
also became involved in the attempts to
increase the K5's range, and came up with the
Pfeilgeschoss, in this case a projectile 120mm (4.7in)
in diameter, 1.8m (6ft) long, with four fins and a form
of rudimentary sabot, which was little more than a
three-part flange, 31cm (7.9in) in diameter, which
was to be fired from a version of the gun with a
smooth-bore barrel bored out to that same calibre.
The sabot flange was discarded as soon as the projectile
was in free flight. With a suitable propellant
charge to take its trajectory well into the stratosphere,
this projectile, which had a 25kg (551b) explosive
payload, reached a maximum range of almost 155km
(95 miles). Development began as early as 1940, but
with a low-grade priority it did not culminate until
1944. Pfeilgeschossen were issued, and seem to have
been used in combat, albeit in small numbers, in
Below: Rheinmetall also built railway guns in 24cm
calibre; this one is seen in northern France, firing at
targets in Kent, across the English Channel.

ARTILLERY
1945. The projectile was the forerunner of the FSDS
(fin-stabilised, discarding sabot) round, now in common
use. The credit for the original idea is usually
accorded to a French gun designer, Edgar Brandt, better
known for the infantry mortars he developed; in
the 1930s he produced a very effective 105mm/75mm
projectile, which had very superior performance
when fired from a 105mm gun with a standard charge.
THE'CROSS-CHANNEL GUN
Meanwhile, Krupp's engineers were also working on
a 'brute force' solution to firing a projectile out to
8()km (50 miles) or more by a simple process of refining
the original design of the Paris Gun. The result
was the K12, in 21cm calibre, which used the same
rifling and shell-seating method as the K5, with the
addition of a composite copper/asbestos/graphite
band to improve its sealing within the tube and maximise
the effect of the propeliant charge. It was hoped
that the use of soft iron splines rather than simple lugs
would both cause them, and not the hardened molybnedum-steel
of the barrel, to wear, and also spread the
load of rotational acceleration, thus prolonging barrel
life even in the presence of an abnormally large pro-
116
peliant charge. The first barrel was proofed in 1937
and the first complete gun, the K12(V), was tested in
1938 and declared serviceable in 1939. It fired a
107.5kg (2371b) shell out to a maximum range of
115km (71.5 miles) and the Army declared itself satisfied,
for it was a greater distance than the Navy had
achieved with the Paris Gun. Beating that record
seems to have been a major incentive. However, it
was less than perfect in operation. It had to be jacked
up by Im (3.3ft) into its firing position, so as to allow
extra space for recoil, and then returned to the lower
position for loading. Krupp was asked to devise an
alternative mounting sub-frame and so produced a
modified gun with strengthened hydraulic buffers as
the K12 (N) in the summer of 1940. No more were
ever constructed.
Mounting the gun presented problems of its own.
To begin with, its barrel was 157 calibres long, well
over three times the length of comparable naval guns,
more than 33m (108ft) from breech to muzzle. This
Below: Two K5s were in action against Allied forces
contained on the beachhead at Anzio for four months in
1944. One was captured and shipped back to the USA.

21CM KANONE 12 (K12)
Calibre: 21.1cm (8.3in)
Barrel length: 33.34m (109.38ft)
Weight (overall): 309,000kg (681,215lb)
Weight of shell: 107.5kg (237lb)
Range: 115km (71.5 miles)
meant that it distorted under its own weight and had
to be very carefully braced. It also needed its trunnions
to be very accurately located at the centre of
balance, otherwise elevation would have been very
difficult. The mount was in the form of an over-size
railway car (more accurately, two railways cars); the
main structure, with the trunnipn supports and elevating
machinery, was mounted on two sub-frames each
of which, in turn, was mounted on a pair of bogies,
two eight-wheeled units to the fore and two tenwheeled
units behind. For operational purposes it ran
on a track section laid in an arc, and it was trained by
running it backwards and forwards. The whole
ensemble weighed 304.8 tonnes (300 tons) and was
over 41m (135ft) long. It appears that the two guns
were operational, with Eisenbahn Batterie 701, only
for brief periods in late 1940 until early 1941, and
they were directed at targets in Kent, particularly
around Dover, from emplacements in the Pas de
Calais. The greatest range attained seems to have
been of the order of 90km (56 miles). One example
was captured by Allied forces in Holland in 1945.
THE HIGH-PRESSURE PUMP
The K12 guns were not the only weapon developed
with an eye to bombarding southern England with
artillery fire, but the other project, the so-called
'High-pressure Pump', was much less conventional,
and relied on a principle first demonstrated, albeit
imperfectly, in the United States of America around
1885. It was the work of Lyman and Haskell, who reasoned
that subsidiary propellant charges, spaced at
intervals up the barrel of a gun in side-chambers and
ARTILLERY
Above: The 21cm K12 railway gun had the longest range
of alf the 'superguns'- around 115km (71.5 miles),
depending on weather conditions.
ignited a micro-instant after a shell had travelled past
on its way up the barrel, would provide a subsidiary
propellant force and thus increase the muzzle velocity
of the projectile. The result, when they built it on
the instructions of the US Army's Chief of Ordnance,
didn't much resemble an artillery piece as we know it.
Firstly, the barrel had to be so long that it could not be
supported save on the ground and had to be laid on an
inclined ramp; and secondly, it had pairs of chambers,
angled back at 45 degrees, let into it for much of its
length. In the event, it didn't work: obturation was
faulty, the flash from the original propellant charge
bypassed the shell and ignited the subsidiary charges
ahead of it, defeating the whole object of the exercise.
Lyman and Haskell gave up, and the idea was consigned
to the history books. It was apparently raised
again in Britian, during World War I, but was turned
down once more.
In 1943, a German engineer named Cönders, who
worked for Röchling Eisen- und Stahlwerke (which
was not just a producer of iron and steel, but had also
been active in the field of munitions) proposed an
identical weapon. Thanks to the success of one of
Cönders' other projects, the so-called 'Röchling
Shell' (a bunker-buster par excellence), those who had
the all-important ear of the Führer, particularly Albert
Speer, the Minister of Munitions, took note. Even
though he would only proceed on the understanding
that no one, not even the HWA, 'interfered' with his
1 1 7

ARTILLERY
work, Cönders was told to produce a prototype of the
Hochdruckpumpe ('High-pressure Pump'). He made
one in 20mm calibre and obtained satisfactory results,
and at that point, Hitler, who had been following
progress with interest, decided to take a hand. Cönders
would, he decided, build not just one or two
guns, but a battery of 50, which would be located in a
suitable position behind Calais, aligned towards London
some 160km (100 miles) away. A suitable site for
what was already being referred to as V3 was found at
Marquise-Mimoyecques behind Cap Gris Nez, very
close to the southern end of the modern-day Channel
Tunnel. This cannot have been altogether easy, when
we consider that the VI and V2 launch sites were
already under construction in that same area. There
must have been, to say the least, a lively discussion as
to which weapon got which piece of real estate.
Despite this, work began on two excavations, each of
which was to hold an array of 25 guns in 15cm calibre,
which would fire long, dart-like projectiles fitted
with stabilising fins, which Cönders was even then
perfecting. Or, more accurately, which Cönders was
not perfecting.
THE HWA TAKES CONTROL
Cönders had built a full-calibre gun at the Hillersleben
proving ground, near Magdeburg, and by late
1943 had run into severe problems, both in putting the
principle into practice and in producing a workable
design for the shell. And even when everything went
according to plan - which was seldom - the results
were not promising, for muzzle velocity, at just over
1000m (3280ft) per second, was nowhere near high
enough. Nonetheless, plans to build a single full-size
gun with a barrel 150m (492ft) long at Misdroy near
Peenemiinde went ahead, while preparation of the site
in the Pas de Calais (now reduced to just one following
a series of successful bombing raids by the RAF
and the USAAF, which had by this time started to pay
very close attention to any large engineering work in
the area) had reached an advanced stage, and a special
artillery battalion was being formed. Still working in
isolation, there was little Cönders could do but press
on and hope for the best. By mid-March, with no
good news coming out of Misdroy, the HWA had had
quite enough of this unconventional working arrangement.
Senior staff travelled to Misdroy for a demonstration
and were less than pleased with what they
saw. Generals von Leeb and Schneider of the HWA
took control. Matters took a distinct turn for the better
as a result. Cönders became but one of the engi-
118
neers working on the three main problems: projectile
design, obturation, and ignition of the subsidiary
charges. In all, six different specialist firms including
Skoda and Krupp produced satisfactory designs for
shells. Obturation problems were solved by placing a
sealing piston between the projectile and the initial
charge, and that in itself solved the problems of precisely
controlling the serial detonation of the subsidiary
charges, for now the flash from the original
charge couldn't get ahead of the projectile and there
was no need to attempt to develop an electrical firing
sequence.
By late May, the Misdroy gun was producing more
satisfactory results, and ranges of up to about 80km
(50 miles) were being reached, when it burst on firing,
destroying two sections. New parts were ordered, and
a further trial set for early July, but meanwhile the
RAF was still at work. After the western site at Marquise
had been abandoned, the Todt Organisation,
responsible for construction, took great pains to hide
the accesses to the eastern site, and for some time it
succeeded. However, by late June, the photographic
interpreters had decided that there was enough evidence
to suggest that something was going on in the
area to justify sending Bomber Command's elite 617
Squadron to pay it a visit with I2,0001b (5443kg)
'Tallboy' deep-penetration 'earthquake' bombs. The
effect of the raid on 6 July was devastating: one bomb
hit the target square-on, and four more scored very
near misses which were actually reckoned to be even
more effective. The site was put out of commission
and no further work was undertaken before it was
overrun by Allied troops.
Meanwhile, on 4 July the trials gun had been fired
again. This time it got off eight rounds - one of which
reached a range of 93km (58 miles) - before it burst,
and that effectively put an end to the project to bombard
London. There is evidence that further development
took place. When Allied troops captured Hillersleben,
they found two guns in damaged condition,
one with 10 pairs of subsidiary chambers (set at rightangles
to the axis of the bore), and the other with five
pairs set at a 45-degree angle. Both were 75m (246ft)
long. There are unsubstantiated reports that two shortbarrelled
versions were built and used in combat
against US forces during the Battle of the Bulge in
December 1944, but experts discount them.
Right: The so-called 'High Pressure Pump' - an innovative
approach to the solution of applying greater propulsive
force to a projectile. It was never effective.

ARTILLERY
11 s

CHAPTER TEN
Tanks and Anti-Tank
Weapons
While the British pioneered the use of armoured fighting vehicles in 1916, by 1939 the
baton had passed to Germany, where men such as Guderian showed that they could
win a war of movement, as British theorists had always promised. Then Hitler took a
personal hand in the German tank programme, and his insistence that size mattered
above all things was to send the entire effort off on a wild goose chase from which it
never fully recovered, even though saner counsel did eventually prevail.
Properly speaking, the tank ceased to be a secret
weapon on the morning of 15 September 1916,
when the British Tank Mark 1, or 'Mother', went into
action on the Somme battlefield. Its appearance came
as a complete surprise to the German infantry, secrecy
having been maintained throughout. Even the
Above: The Panzerjäger Tiger was based on the vehicle
Ferdinand Porsche put forward for the Tiger project.
Left: The 'Panzerschreck' fired a rocket-propelled grenade
with a hollow-charge warhead.
name 'tank' was deliberately misleading, though it
stuck. More of a secret than the existence of tanks in
the German Army was the way in which they would
be employed. In any event, their use came as a complete
surprise to the Poles in 1939 and to the French
the following year. However, that was not to say that
new models would be developed in full view.
THE TIGER TANK
When the 58-tonne (57-ton) Sonderkraftfahrzeug
(SdKfz) 181 Panzerkampfwagen VI Tiger first went
into action on the Leningrad front, 26 years ancf 1 day
121

TANKS AND ANTI-TANK WEAPONS
PzKpfw VI TIGER Ausf E
Length (overall): 8.24m (27.00ft)
Width: 3.73m (12.25ft)
Weight: 58,000kg (127,867lb)
Max road speed: 38km/h (24mph)
Max road range: 100km (60 miles)
Crew: 5
Armament: 8.8cm KwK 36 gun;
2 x 7.92mm MG 34 machine guns
after the armoured fighting vehicle made its original
debut, it was something the like of which had never
been seen. With frontal armour 100mm (3.93in) thick,
it was unstoppable at anything but suicidally short
range, and its 8.8cm/L56 gun could, quite literally,
shoot straight through any vehicle it might happen to
meet, the Soviet T-34 which it was specially built to
combat being no exception.
In fact, the Tiger's first outing was indecisive, and
its second, a week later, much less than successful
when one of them bogged down in no-man's-land and
had to be blown up to prevent it from falling into
enemy hands. It was January of the following year
before Tigers went into battle again, and it soon
became clear that they were not the omnipotent force
they had been thought to be, even though at best, and
in the best hands, they were very effective indeed. In
the long run, the Tiger would prove to be deeply
flawed: its fuel consumption was shocking, and its
powerplant and transmission insufficiently robust. By
1944, the Allies had weapons capable of dealing with
it, but it seems to have had a place second to none in
Adolf Hitler's affections. Certainly it fulfilled all his
'biggest ... strongest... best' requirements, at least in
the short term. It was eventually to be superseded by
the 71.1-tonne (70-ton) SdKfz 182 Tiger II, which
was more of everything, and which, despite being
even less effective in all but very narrowly defined circumstances,
still did not prove to the Führer that the
law of diminishing returns was at work.
THE GIANT MOUSE
Hitler is usually held responsible for the decision to
build the monster tanks, and he certainly gave them
his very active personal approval, but he had a willing
122
Above: The Tiger was the first of the German 'supertanks',
and was effective if properly handled. Its underpowered
engine was the cause of many breakdowns, though.
assistant in the person of one Dr Ing. Ferdinand
Porsche, who, conveniently, was both the country's
leading tank designer (at least, in his own eyes) and
head of the Tank Commission. As early as 1942, even
before the Tigers had gone into action, Porsche
brought forward a plan for a tank he called, presumably
with studied irony, the 'Maus' ('Mouse'). This
was to be a 152.4-tonne (150-ton) vehicle, with
frontal armour a massive 350mm (13.75in) thick, and
mounting either a 12.8cm or a 15cm gun with a 7.5cm
gun mounted co-axially (as well as a 2cm cannon and
two 7.92mm machine guns). Like Porsche's proposed
design for the Tiger (which became the Panzerjäger
Tiger), the 'Maus' was to have petrol/electric drive, its
1200bhp engine driving a generator, which in turn
drove electric motors in the hubs of the driving
wheels. This was an elegant enough solution to the
many problems of power transmission, but one which
would ultimately prove to be flawed, at least on this
smaller scale. Submarines and even battleships used it
successfully, but in tanks, the motors were not powerful
enough and drivers often burned them out trying to
extricate their vehicles from difficult situations.
Orders were placed for six prototypes, the first of
which was mobile under its own power in December
1943. It proved surprisingly successful, attaining a
speed of 20km/h (12.5mph) with an under-spec
lOOObhp engine; particularly successful was its suspension
system, which was a modified version of
Porsche's Tiger's, with longitudinal torsion bars and
four interleaved roadwheels per stub-axle. At a total

PzKpfw VI TIGER H Ausf B
Length (overall): 10.26m (33.66ft)
Width: 3.75m (12.29ft)
Weight: 71,100kg (156,747lb)
Max road speed: 38km/h (24mph)
Max road range: 110km
(68 miles)
Crew: 5
Armament: 8.8cm KwK 43 gun;
2 x 7.92mm MG 34 machine guns
weight of almost 193 tonnes (190 tons) including its
six-man crew, fuel and ordnance, there was hardly a
road bridge in the country which would have taken its
weight, and thus it was designed from the outset to be
able to submerge to a depth of 8m (26.25ft), air for
occupants and powerplant being supplied via a
schnorkel tube which extended from the turret roof.
The 'Maus' project didn't get much further than the
initial stage; in all, nine prototypes had been wholly
or partially completed by the war's end, though that
Below: A pair of knocked-out Tigers in the Soviet Union in
1944. By that time the Allies had got the measure of these
58-tonne (57-ton) monsters.
TANKS AND ANTI-TANK WEAPONS
Above: The King Tiger was heavier than the Tiger and had
a more powerful 8.8cm gun. It was, however, also prone
to breakdowns, having the same powerplant as the Tiger.
small result does not reflect the amount of energy,
money and scarce resources which had been lavished
on it. And worse was to come, because the HWA -
having protested that it did not want such a vehicle
and could formulate no sensible tactical plan for its
use, and having been overruled by the Führer - then
decided to commission something very similar itself!
It comes as no surpise to find that it was to Henschel,
the producer of both versions of the Tiger (and
of the much more successful PzKpfw V Panther), that
1 93

TANKS AND ANTI-TANK WEAPONS
PANZER 'MAUS'
Length (overall): 10.08m (33.08ft)
Width: 3.67m (12.00ft)
Weight: 193,000kg (425,488lb)
Max road speed: 20km/h (12.5mph)
Max road range: 190km (119 miles)
the HWA turned, and even less of one to learn that the
E100, as the project was known, displayed more than
a passing resemblance to them, though it was certainly
on a grander scale. Its all-up weight was estimated
at 142.2 tonnes (140 tons) which would probably
have meant it going into battle at least 10.16 tonnes
(10 tons) heavier, and it, too, was to have had the
KwK 44 15cm gun and a co-axially mounted 7.5cm.
In all, it appears to have been a more realistic (though
the phrase is used loosely) proposition than the Maus.
One prototype was under construction at the war's
end, but had never run.
In all, the German tank development programme
during World War II was deeply flawed by the
assumption that a single vehicle, heavily armoured
and with a powerful gun, would be able to out-fight
(or at least out-range) any number of enemy tanks. By
the time the Allies landed in Normandy in 1944, this
was certainly not true. American Sherman tanks,
which appeared on the battlefield around the same
time as the Tiger, had by then acquired very much
more powerful guns - the 76mm in Americanmanned
tanks, the 17pdr in British service - and had
a fighting chance which their numerical superiority
turned into a certainty. The same was true in the east
with the up-gunned T-34. It would have been very
much more sensible to have abandoned the Tiger (or
better still, never to have begun it) and to have concentrated
instead on the PzKpfw V Panther, which
many experts rate as the best tank of the entire war.
Certainly, Panthers were quicker (and much cheaper)
to produce, and were formidable opponents, with a
124
Crew: 6
Armament: 15cm KwK 44 gun, 7.5cm KwK 44
gun; 2 x 7.92mm MG 34 machine guns
Above: Even the King Tiger would have been dwarfed
beside the 'Maus'. Its secondary armament was to have
been the 7.5cm gun, the Panther tank's main armament.
KwK 42 7.5cm cannon, 70 calibres long, developed
by Rheinmetall-Borsig, which was capable of perforating
any Allied tank at virtually all ranges.
ANTI-TANK WEAPONS
If the German tank development programme was
fatally flawed, the same could not be said of the antitank
(AT) weapons development programme. At the
start of World War II, anti-tank weapons were simply
not up to the task, save in a few particulars. One was
the heavy German 8.8cm gun, which had started life
as an anti-aircraft weapon but which showed itself
during the Spanish Civil War as a very successful AT
weapon, once appropriate armour-piercing projectiles
had been developed. It soon acquired a practical and
practicable mobile mounting, and was issued as the
Panzerabwehrkanone (PaK) 36; it was also adopted as
the KwK 36 for the Tiger tank. It was very capable,
but entirely conventional; other German developments
in high-velocity guns intended for use against
armoured vehicles were not.
THE TAPERED-BORE GUNS
The earliest suggestion for a gun with a uniformly
tapering barrel seems to have originated in Germany
in about 1903 with a man named Karl Puff. He suggested
using a projectile with a sleeve, which was
compressed by the taper of the bore until it filled a

series of grooves in the body of the bullet. By that
means, the velocity of the projectile was much
increased, since its cross-sectional area had been
diminished considerably while the pressure in the barrel
remained constant (the velocity being a product of
the two). Unfortunately for Puff, the complexities of
manufacturing a rifled tapered bore were beyond the
capability of German gunmakers, and nothing came
of the idea, at least, not then.
In the 1930s, another German, a gunmaker named
Hermann Gerlich, experimented with Puff's scheme,
and was able to manufacture hunting rifles according
to the principle. They proved to be excellent, with the
all-important flat trajectory, but when he tried to interest
the armed services of a number of countries in
such a rifle, he was less successful, entirely, it seems,
thanks to the projected cost of the weapon. However,
the Springfield Arsenal, for one, certainly validated
the concept, producing a version of the M1917 rifle
with a muzzle velocity of over 2135m/s (7000ft/s)
instead of the standard 855m/s (28QOft/s). Gerlich
gave up trying to market the concept himself in 1933,
and contacted Rheinmetall, who saw the possibility of
incorporating the system into an anti-tank rifle, using
a projectile with a tungsten carbide core and soft steel
skirt. Eventually, it produced what became known as
the Panzerbüchse (anti-tank rifle) 41, which fired a
20mm (it had started out at 28mm nominal diameter)
round at a muzzle velocity of around 1400m/s
(4600ft/s), and which could perforate (ie, pass completely
through) 66mm (2.6in) of nickel-steel armour
at a range of 500m (1640ft). Soon, Rheinmetall produced
a more powerful version in 4.2cm nominal calibre,
which squeezed its projectiles down to 29.4mm,
and which could perforate that same thickness of
armour plate at twice the distance. It entered service
in 1941 as the 4.2cm Panzerabwehrkanone (anti-tank
gun) 41, and proved to be very successful.
THE SQUEEZE-BORE GUN
Two years earlier, Krupp had also begun to examine
the possibilities of reducing the cross-sectional area
of a projectile while it was in the barrel, and settled on
a slightly simpler, but no less effective, method of carrying
out the procedure. Instead of manufacturing a
barrel with a uniformly tapered bore, Krupp added a
smooth-bore, step-tapered section to the muzzle of a
conventional gun. The (flanged) round entered the
supplementary section at nominal diameter of 7.5cm
and passed through two tapered sections which
reduced it to 5.5cm. The advantage of this was chiefly
TANKS AND ANTI-TANK WEAPONS
Above: The 8.8cm Raketenwerfer 43, usually called the
'Püppchen', was not a gun but a rocket launcher. It was
superseded by the shoulder-held tube rocket launchers,
logistical; only the unrifled, tapered section became
badly worn (that, of course, was the system's great
drawback), and was attached to the main section of
the barrel by a simple screw collar, which meant it
could be replaced in the field without the need for
special tools. The 7.5cm PaK 41, as the gun was
known, fired a tungsten-cored shot weighing 2.6kg
(5.71b) at a muzzle velocity of 1125m/s (3700ft/s) and
could perforate 125mm (4.9in) of armour, more than
any tank had, at a range of 2000m (6560ft). This gun
was the weapon originally specified for the Tiger
tank. The taper-bore and squeeze-bore guns were
without question excellent battlefield weapons, but
they needed tungsten for their bullet cores if they
were to be effective, and that was a material in short
supply in Germany at that time, being much in
demand in the engineering industry as cutter bits for
machine tools. Eventually, a choice had to be made,
and the manufacturing industry won. The taper-bore
and squeeze-bore guns were taken out of service and
scrapped and few survived the war. Rheinmetall and
Krupp offered conventional anti-tank guns in larger
calibres instead, culminating in the 12.8cm PaK 44.
SHAPED AND HOLLOW CHARGES
The kinetic energy of a very hard object travelling at
high speed (brute force, in other words) was one way
to perforate armour, but there was another; the shaped

TANKS AND ANTI-TANK WEAPONS
Above: The Panzerfaust 30 was the simplest of all German
rocket-propelled grenade launchers. Its designation
referred to its optimum range - 30m (32.8 yards).
Below: Appearances are not deceptive. The
'Panzerschreck' was developed from the US Bazooka,
and was just as effective. Two versions were produced.
126
or hollow explosive charge, which incorporated a hollow
cone or hemisphere of metal translated by the
heat of the explosion behind it into a high-speed
(around 7500m/s; 24,600ft/s) jet of molten material
and gas. This was first produced, in Germany in 1939,
as a demolition charge, and is reputed to have been
first used in combat at the storming of the fortress of
Eben-Emael in May 1940. By that time, however, its
developers had moved on, and were on the verge of
producing an artillery shell on the same principle.
The British and Americans had also made considerable
progress independently, while the Soviets had
achieved the same ends by the rather simpler means
of copying captured or stolen German munitions.
However, in this principle, there was a problem: the
act of spinning the shell to maintain its accuracy in
flight dispersed the molten jet and made it much less
effective. One answer was to stabilise the round with
fins instead, but that took some working out. Another
answer was to emulate the pyrotechnic 'sky rocket'
and fit the projectile with a long shaft for a tail. In the
successful German development of this simple principle,
the rod was surrounded by a tube upon which fins
were mounted. The rod went down the barrel of a
3.7cm PaK 36 anti-tank gun, and the tube fitted
around it, with the shaped-charge warhead, with its
copper hemisphere and 2.4kg (5.31b) of TNT and hexogen
sitting in front of the mu/zle. It was propelled by

PANZERFAUST 30
Projectile diameter: 150mm
(5.91in)
Weight (overall): 5.22kg
(11.5lb)
Range: 30m (32.8 yards}
Penetration: 200mm (7.87in)
a special cartridge, loaded conventionally at the
breech, and was reasonably accurate up to about
300m (985ft). Being independent of the kinetic energy
of the round in flight (which diminished with distance,
of course) the warhead was equally effective at
all ranges, and could pierce 180mm (7.08in) of
armour. The shaped-charge warhead was also to be
mated with simple solid-fuel rocket 'motors' to produce
early RPGs (rocket-propelled grenades), the
Panzerfaust and the Raketenpanzerbüchse (also
known as the 'Panzerschreck' - 'panzer terror'),
which was a direct copy of the American Rocket
Launcher M l, the celebrated Bazooka, using German
8.8cm rockets.
THE RUHRSTAHL X-7 'ROTTKÄPPCHEN'
An altogether more elegant solution to the problem of
killing tanks on the battlefield at something greater
than suicidally close quarters (the main problem with
the Panzerfaust and 'Panzerschreck') was put forward
by Ruhrstahl. We have already encountered this company
as the producers of the 'Fritz-X' guided bomb
and the X-4 air-to-air guided missile, in response to
HWA's request in 1944. The X-7 'Rottkäppchen'
('Red Riding Hood') was essentially similar in nature
to the X-4 AAM, with its conventional HE warhead
exchanged for a 2.5kg (5.51b) shaped charge, and with
its control system cunningly simplified. Like the X-4,
the X-7 was winged (two wings only, in this case,
with parabolic leading and trailing edges, with spools
from which the control wire paid out located at their
tips) and revolved slowly in flight, both pitch and yaw
TANKS AND ANTI-TANK WEAPONS
RPzB 43 'PANZERSCHRECK'
Calibre: 88mm (3.46in}
Length: 1.638m (5.375ft)
Weight (overall): 13.12kg
(28.86lb)
Range: 150m (164 yards}
Above: The Raketenpanzerbüchse 43 'Panzerschreck' and
the simpler Panzerfaust gave even individual infantrymen
the means to kill tanks.
being controlled by a single spade-like vane or fin
mounted at the end of a curved arm which, when the
missile was launched, hung down and behind the
body. As the missile rotated (once again, at a rate of
about one complete turn per second), this was able to
exercise control over both pitch and yaw, a gyroscopic
switch transferring the signals to actuate the simple
spoiler as it turned from the vertical to the horizontal
plane and so on, an elegant solution indeed.
The X-7 was powered by two WASAG solid-fuel
rockets whose diglycol propellant was in the form of
two concentric tubes. The first charge gave a thrust of
68kg (1501b) for two and a half seconds to launch the
missile into flight and get it up to its 360km/h (224
mph) operating speed; the second gave 5.5kg (121b)
of thrust for eight seconds (which was actually longer
by a considerable margin than the flight was likely to
last) to sustain it. Maximum range was to have been
around 1200m (1310 yards). It is thought that a total
of a few hundred Ruhrstahl X-7s were manufactured,
and that most were consumed in testing, but there is
some evidence to suggest that some made it into the
field, and were expended in combat on the Eastern
Front during 1945. There are unconfirmed reports that
the X-7 performed satisfactorily, and was able to deal
even with the JS-1 'Stalin' heavy tank, which was
impervious to virtually everything else at anything
over short range.

CHAPTER ELEVEN
Submarines and
their Weapons
By the time World War II was halfway through, Germany (and in particular the Führer
himself) had largely given up on its surface navy, but the submarine arm was another
matter entirely. U-boat veterans knew, however, that much still remained to be
developed in the boats themselves, and a well-funded programme was put into
effect. Yet again it proved to be just too late, however, for by the time the newgeneration
boats were coming off the ways, the war was already lost.
If the Luftwaffe was the Nazi Party favourite in prewar
and wartime Germany, the Kriegsmarine
(Navy) was, for a variety of reasons, very definitely
not. Some of the reasons were historical and political,
and went back to the dark days of near civil war in the
1920s, but others were more recently rooted, and had
to do exclusively with the poor performance of
German capital ships. At one point, an enraged Hitler
actually ordered all the surface fleet to be scrapped.
The exception was the submarine service which,
under the talented leadership of Karl Dönitz, had
Above: The Type XXI U-boat was one of the most
influential naval developments of the twentieth century.
Left: Germany also developed midget submarines, like this
'Biber' putting to sea from Rotterdam at Christmas 1944.
actually come close to cutting Britain's vital lifeline
to the United States and to its colonies. Most of the
few funds for development that did find their way to
the Kriegsmarine were destined for the U-boat arm.
HOMING TORPEDOES AND MAGNETIC MINES
By the end of World War I, the submarine torpedo, the
first really successful model of which had been produced
by the Anglo-Italian Whitehead in 1868, had
been developed to the point where it was a reliable,
practical weapon. During that war it had been used to
sink thousands of ships (German submarines alone
accounted for 5556), and we can hazard a guess that
the individual success rate (expressed as hits per torpedo)
probably made it one of the most effective
offensive weapons of the whole conflict. However, it
was a relatively simple, unsophisticated weapon, and
129

SUBMARINES AND THEIR WEAPONS
that, combined with its effectiveness, surely meant
that it could be improved. There was certainly the
possibility of giving it much greater endurance and
straight-line performance, but increasing the range
always resulted in a lowering of the strike rate, since
the torpedoes had no self-directive capability. There is
reason to believe that scientists in Germany had actually
perfected a passive acoustic homing device to
steer a torpedo towards a submarine sound source by
1936, and that the new weapon had been kept back
from production to preserve its secrecy.
FOXING THE 'FOXER'
The relatively simple first-generation devices, which
were restricted to fairly low speeds, proved effective
against slow-moving targets such as merchant ships,
but less so against warships, which often simply outpaced
them. Towed noise-makers (known as 'Foxers';
originally no more than two lengths of iron pipe,
Below: U14Q6, one of the few operational Type XVII
Walter-engined boats to be completed. She was scuttled
in May 1945 but was salvaged and taken to the United
States. A sister-boat, U1407, went to the UK.
30
chained loosely together so that they constantly
crashed into each other) could also dupe these
devices, and it was September 1943 before German
scientists perfected a means of outwitting them.
When a torpedo fitted with the second-generation
T5 or 'Zaunkönig' ('Wren') passive acoustic seeker
detected a sound source in a small arc ahead of it, a
subsidiary circuit operated a simple solenoid switch
to actuate the small rudder vane. This caused the torpedo
to turn sharply to starboard and run in a circular
path for a predetermined period (long enough, in fact,
for it to describe a semi-circle) before turning sharply
to starboard once more and setting off on its original
track again. In this way, the torpedo skirted the noisemaker
and homed in on the propeller noise of the ship
towing it instead. Then, on encountering the noise of
the ship dead ahead, the torpedo turned to perform the
circling manoeuvre once more. The diameter of the
semi-circular track the torpedo described being less
than the length of the ship plus the distance the latter
covered in the intervening period, it would strike the
target from the beam. It has been estimated that 700
T5s were fired in anger, and that 77 (11 per cent)
scored hits. The US Navy introduced the similarly

TYPE XVIIB
Type: Coastal submarine
Displacement: 317 tonnes (312 tons) surfaced;
363 tonnes (357 tons) submerged
Length: 41.50m (136.17ft)
Submerged speed: 21.5 knots
equipped Mark 27 torpedo in 1944, and in the last
years of the war, 106 were fired in combat, scoring 33
hits (31 per cent).
Another approach was to fit a form of automatic
pilot, which caused the torpedo to make a series of
pre-programmed turns after it had run a preset distance,
in the hope that a torpedo fired in the general
direction of a convoy would turn and hit a ship purely
by chance. Neither the success rate of the
Federapparat-Torpedo, nor that of its more sophisticated
successor, the Lagcnunabhangiger-Torpedo
(which could be fired from depths of up to 50m;
164ft), seems to have been recorded. Later U-boats
had their six forward-facing torpedo tubes organised
into an array which covered 10 degrees of arc; firing
all six in a salvo gave a much-improved chance of hitting
the target. It is obvious that the same guidance
system which was applied to the glider bombs and the
guided missiles could also have been applied to torpedoes,
even though keeping a precise track of the
missile's course would naturally have been more difficult.
It is inconceivable that an experimental programme,
at least, was not initiated. Certainly, one of
the Kriegsmarine's original submarine warfare
instructors, Werner Fürbringer, suggested it.
A viable alternative to the torpedo was to lay mines
in the path of the oncoming enemy (particularly if this
was a slow-moving convoy), and a variety of submarine-launched
mines were developed. The Torpedo-
Ankertaumine (TMA) had a 215kg (4751b) explosive
charge, and was attached to an anchor which allowed
it to float at a predetermined height, while the
Torpedo-Grundminen lay on the seabed in shallower
water. They came in two sizes: the 500kg (llOOlb)
TMB and the 1000kg (22001b) TMC. All three mines
were dimensioned to allow them to be deployed
SUBMARINES AND THEIR WEAPONS
Submerged range: 210km (130 miles)
Armament: 2 x 533mm (21 in) torpedo tubes
Crew: 1,9
Above: The Type XVII boats had both conventional diesel
engines and a single Walter closed-cycle engine. They
were designed for coastal operations.
through a standard 533mm (21in) torpedo tube and
could be fitted with a variety of remotely actuated detonators,
magnetic or acoustic.
THE NEW GENERATION OF SUBMARINES
There was little development of the basic submarine
in the inter-war period, except that the once-popular
saddle-tank design, in which the buoyancy chambers
were located outside the pressure hull, gave way more
and more to the double hull, in which they enclosed it
almost completely and were themselves contained
within a light enclosure which could be shaped to
improve sea-keeping and performance. In Germany,
developments in the late 1930s were aimed only at
increasing the size and endurance of existing types,
not making any radical changes to their design.
However, by 1941, experimental boats with a new
type of powerplant which did not need atmospheric
oxygen had been produced, and were proving to be
quite remarkable. The powerplant in question was,
once again, the creation of the prolific Professor
Hellmuth Walter, whom we have already met.
Walter had constructed a small experimental boat,
the V30, launched on 19 January 1940, which displaced
just 73.8 tonnes (75 tons) submerged. He
equipped it with a steam turbine, fed by a variant of
the liquid-fuel motors which were to power the VI
flying bomb's launch catapult, producing their steam
by the chemical reaction of hydrogen peroxide with a
catalyst. Walter soon discovered that his submarine
could make almost 30 knots submerged - around
three times the submerged speed of any conventional
131

SUBMARINES AND THEIR WEAPONS
TYPE XXI A
Type: Ocean-going submarine
Displacement: 1620 tonnes (1595 tons) surfaced
1848 tonnes (1819 tons) submerged
Length: 76.70m (251.66ft)
Submerged speed: 17 knots
Above: The Type XXIs were ocean-going submarines of
over 1600 tonnes (1575 tons), the size of a small destroyer
of the period. They could make 17 knots submerged.
submarine running on battery power - and that led
him to suggest to the Kriegsmarine the construction
of a fleet of similarly powered submarine warships.
When asked where he proposed to store the large
quantities of reagent and fuel that would be required,
he produced a design for a two-decker submarine, in
itself virtually two existing double hulls joined into a
tigure '8', the bottom portion of which would serve
132
Submerged range: 525km (325 miles) at 6 knots
Armament: 6 x 533mm (21 in) torpedo tubes;
4 x 20mm AA guns
Crew: 57
exclusively as 'bunkerage'. Someone at this proposal
meeting noted that it would be just as easy to fill that
lower section with batteries.
THE'ELECTRO-BOATS'
Whatever the method adopted, as the war wore on, it
was to become harder and harder for U-boat commanders
to remain on the surface, even at night,
Below: The conning tower top of a (scuttled) Type XXI.
Note the retractable radio antenna and the faired-in
machine gun emplacements.

TYPE XXIII
Type: Coastal submarine
Displacement: 233 tonnes
(230 tons) surfaced; 260 tonnes
(256 tons) submerged
Length: 34.7m (113.75ft)
Submerged speed: 22 knots
Above: The other 'Electro-boats' were the much smaller
Type XXIIIs, intended for coastal operations. Even with a
complement of just 14, they were cramped, much of the
interior being given over to batteries.
thanks to the increasingly effective airborne anti-submarine
patrols mounted by the RAF and the USAAF.
If they were to continue to wage war effectively, they
would have to be provided with boats which could
stay submerged for extended periods and perform
more effectively under water, and it was along these
lines that the bulk of research was carried out. More
'Walter' boats were built or at least were in the course
of construction when the war ended. The two Type
XVIIB boats which were successfully salvaged after
having been scuttled in Hamburg harbour were later
transferred to the US Navy and the Royal Navy, who
operated them experimentally, but the powerplant
required massive quantities of fairly exotic fuel and
was most temperamental. It would perhaps become a
valid solution in the fullness of time, but that was
something the Kriegsmarine did not have, and it was
essential to look at other suggestions.
THE TYPE XXI AND TYPE XXIII
The off-the-cuff remark to Walter about using the
lower-deck space of his two-deck submarine for batteries
was to have far-reaching consequences, and to
lead to the construction of two classes of submarines
which were actually faster submerged than they were
on the surface: the ocean-going Type XXI; and the
smaller, coastal Type XXIII. They were not the first to
so perform; right at the end of World War I, the British
constructed a class of 'hunter-killer' submarines, the
'R' class, with the 220-volt batteries taken from the
much bigger T class, combined with a spindle-form
SUBMARINES AND THEIR WEAPONS
Submerged range: 325km
(202 miles) at 4 knots
Armament: 2 x 533mm (21in)
torpedo tubes
Crew: 14
hull from an earlier era, with a speed on the surface of
9.5 knots and 15 knots submerged. They proved to be
difficult to control, and were stricken prematurely,
though R4 stayed in service until the early 1930s.
The two types of German combat submarines were
quite different in character. The Type XXI11 was
strictly for local deployment in coastal waters, if only
by virtue of its size. It displaced 233 tonnes (230 tons)
on the surface, was 34.7m (113.8ft) long and 3m
(9.8ft) abeam, and had a crew of just 14. Its biggest
weakness as a warship was that it carried just two
533mm (21 in) torpedoes, pre-loaded into two bow
tubes, and no re-loads. Almost 500 were scheduled to
be built at yards in Germany (Kiel and Hamburg),
France (Toulon), Italy (Genoa and Montefalcone),
and Russia (Nikolaev), but only the German yards of
Deutsche Werft and Germaniawerft actually launched
any boats, the German Army having been driven back
out of occupied territory before any could be completed.
The first boat, U2321, was launched at
Hamburg on 17 April 1944 and a total of 63 had been
completed by the time the war ended. However, problems
of commissioning meant that only 10 operational
patrols were made from March to May 1945;
six merchant ships were sunk, two of them, by
U2336, off Scotland on 7 May, being amongst the last
sinkings of the war.
As its powerplant, the Type XXIII had a single
580bhp MWM diesel engine which drove two electric
motors either directly or via the extensive batteries.
The principal electric motor produced 580shp and
could produce a submerged top speed of 22 knots; the
secondary, 'creeping', motor produced just 35shp for
a speed of 5 knots, but in almost complete silence.
Using the secondary motor alone, the submarine
could stay submerged, making a speed of 4 knots, for
1 33

SUBMARINES AND THEIR WEAPONS
134
40 hours. Like the bigger, Type XXI boats, they were
streamlined in appearance, with all external fittings
either faired-in or removed.
The Type XXI was a more sophisticated boat than
the Type XXIII; it was 76.7m (251.6ft) long and 6.6m
(21.6ft) abeam, displacing 1620 tonnes (1595 tons) on
the surface. Type XXIs were equipped with six torpedo
tubes, all of them situated in the bow, and a total of
23 torpedoes (they were also to have carried four
30mm anti-aircraft cannon, but never did, a pair of
20mm cannon being substituted). Like the coastal
boats, they were double-decked, the frames being fitted
outside the pressure hulls, which suited the modular,
prefabricated building method by then in use in
Germany. Their powerplants were considerably more
powerful, of course: they had two MAN diesels of
lOOObhp each driving two propeller shafts via two
125()shp electric motors or two 57shp 'creeping 1
motors; on the surface they could make 15.5 knots
and submerged, on main engines, over 17 knots, with
5 knots available from the auxiliary motors.
Almost 700 Type XXIs were scheduled to have
been built by Blohm & Voss in Hamburg, Deschimag
in Bremen, and Schichau in Danzig (Gdansk), but
only 121 were actually commissioned. Many more
were bombed on the slip prior to launching and a substantial
number remained incomplete at the end of the
war. Some of them - and some of the boats already in
commission - were taken to the Soviet Union and
completed there and formed the backbone of the Red
Navy's submarine arm for many years. Indeed, so
greedy were the Soviets for German submarines that
they loaded the hangar decks of the incomplete hull of
the aircraft carrier Graf Zeppelin with U-boat hull
sections and proceeded to tow it the length of the
Baltic to Leningrad, but it hit a mine in the Gulf of
Finland and sank. Only two Type XXI boats ever left
port on operational patrols and neither fired a shot in
anger. The advance in submarine operations which
the Type XXI and Type XXIII represented cannot be
overstated. They altered the world's navies' perceptions
of what could be expected of a submarine, and
every design later produced, up to the modern
'teardrops', reflected that.
Left: The head of an extensible induction mast, or
schnorkel tube. It took considerable ingenuity to produce
a self-regulating valve system which was fast-enough
acting to prevent large quantities of water being sucked
into the submarine. The Dutch were the first to find a
solution to the problem in about 1936.

Above: A 'Marder' ('Marten') midget submarine being
launched by crane. The nature of the craft-it was no
more than a torpedo with a small crew compartment
replacing the warhead - is obvious.
Below: The 'Molch' ('Salamander') was slightly more
sophisticated than the 'Marder'. It carried two underslung
torpedoes and around 400 were built The 'Molch' was
used against Allied shipping in the Scheldt.
SUBMARINES AND THEIR WEAPONS
THE SCHNORKEL
There was one more way to keep the boat submerged
with its engines running, of course: let it breathe
through a tube. This may seem an obvious solution,
and indeed, the very earliest submariners had adopted
it, but in a large boat travelling even at only 5 or so
knots, a breathing tube was very difficult indeed to
maintain in operation in anything but a flat-calm sea.
The practical problems were largely solved, however,
by about 1936, and in a somewhat unlikely quarter:
the Netherlands. When the German Army invaded in
May 1940, examples of submarines with functional
extensible induction masts (as the breathing tubes are
properly known) were captured intact, but were never
copied, and those fitted to Dutch submarines which
the Kriegsmarine put into operation were removed.
German submarine commanders 1 policy was to
remain on the surface as much as possible, and only
submerge to avoid escape or to make a particularly
risky attack. As a result, U-boat commanders had no
use for the snorting mast, at least, not until the dark
days of 1943, when they were regularly being forced
to dive by anti-submarine patrols, and when a
research programme was put in hand to replicate the
135

SUBMARINES AND THEIR WEAPONS
results the Dutch had achieved. The first German submarine
to have been fitted with a schnorkel seems to
have been U264, and she was lost in February 1944
during her initial attempt to use it. Some experts
maintain that the first-generation schnorkels caused as
many problems as they solved, but they achieved their
major objective of allowing the submarine to run submerged
on its diesel engines, even if was a tricky
business, and unpopular with the crew, who had been
accustomed to a short watch on deck every now and
then. Tt could also be very dangerous, as the loss of
U264 indicates, as it was all too easy to run the headvalve
(a simple ball valve at the end of the U-shaped
top section of the induction tube) under water, whereupon
the diesels would begin to suck the air out of the
boat's interior and would create a very considerable
under-pressure before they stopped.
MIDGET SUBMARINES
Given their almost complete lack of success, it comes
as something of a surprise to discover the extent of the
German Navy's midget submarine programme. At
least six different types of craft were produced in considerable
numbers - certainly over 1500 in total -
from 1943 (the programme was behind those of
136
Britain, Italy, and especially Japan). The first types
would more accurately be called semi-submersibles,
for they all ran with their upper surfaces barely
awash, the solitary crewman being able to see out
through ports in the vestigial conning tower which
enclosed his head. The first constructed was known as
the 'Hecht' (Tike'); it was battery-powered and really
little more than a manned torpedo with a detachable
warhead. An improved model, the 'Neger'
('Negro') had a petrol engine, and carried an underslung
torpedo. Tt worked well enough, but its solitary
crewman had to breathe oxygen, and was thus
restricted in what he could do. Two larger one-man
types, the 'Molch' ('Salamander') and the 'Marder'
('Marten'), were slightly more practical, with recirculating
air supplies. The former carried two underslung
torpedoes, and was used with some success against
Allied shipping in the Scheldt in late 1944 and 1945.
The 'Marder' carried just one torpedo but could submerge
completely in order to attack.
Below: The 'Biber' ('Beaver') was the third one-man
midget submarine type. It could be transported by road or
by specially equipped 'mother' submarines and proved to
be quite successful in 1944-45.

The next step was to produce a true submersible, a
proper submarine in miniature. The first attempt
resulted in a single-seater experimental vehicle called
the 'Hai' ('Shark'), powered by a petrol engine and
batteries, which could make 20 knots for two hours on
its electric motor. The 'Hai' was developed into the
one-man 'Biber' ('Beaver'), which displaced 3.04
tonnes (3 tons) and carried two torpedoes slung
beneath the hull; a later version of the 'Biber' was
capable of carrying a second crewmember. Over 300
were built and used with a measure of success in the
Scheldt Estuary and off Murmansk in the convoy
assembly area. The 'Biber' could be transported by
road or by air as well as by specially modified conventional
submarines.
SUBMARINES AND THEIR WEAPONS
Above: The best of all the German World War II midget
submarines was the two-man 15.2-tonne (15-ton)
'Seehund' ('Seal'), the only type which was truly capable
of operating independently.
The most successful of the German midget submarines
was the two-man 'Seehund' ('Seal'). This
was much bigger at 15.2 tonnes (15 tons) displacement,
and had jettisonable auxiliary fuel tanks, which
gave it a range of around 800km (500 miles). It could
make 8 knots on the surface and 6 knots submerged.
The 'Seehund' also gained some success in the mouth
of the Scheldt. Unconfirmed reports from German
sources claim that it also operated against merchant
shipping in the Thames estuary and off Margate.
37

CHAPTER TWELVE
Nuclear, Biological
and Chemical
Weapons
When war broke out in 1939, it was feared that poison gas would be used even more
widely than it had been in World War I. To that fear was added the threat of
biological agents, while physicists were struggling with the possibility of harnessing
nuclear fission to produce a bomb the likes of which had never been seen.
In December 1938, German physicists Otto Hahn
and Frit/ Strassman demonstrated the fission (splitting)
of the uranium atom. This caused a stir in the
scientific community, and ripples spread outside it,
even as far as the HWA, to which several scientists
wrote, suggesting that the phenomenon might conceivably
be used in a bomb. The notion made slow
progress, but by late 1939 a steering committee had
Above: The Heinkel He 177A-5; an He 177 was modified to
carry the never-completed German atom bomb.
Left: A US serviceman is confronted by massed ranks of
German mustard gas shells afterthe war.
been formed. It had just one item on its agenda: could
a nuclear reactor to produce fissionable material be
built? As a rider, subsidiary questions were posed
about costs and timescale. A research programme was
drawn up, and six university-based projects were
established. By 1941, it had become clear that the
notion was feasible, and the steering committee
reported to HWA that a reactor could and should be
built, and that it should use as its moderator, deutrium,
also known as 'heavy water'. The entire project
went downhill from there, but it would be a long
while before that was to become obvious. By 1942,
five different laboratories were experimenting with
atomic piles, each one with a different theory of how
39

NUCLEAR, BIOLOGICAL AND CHEMICAL WEAPONS
it should be constructed, and each one in ignorance of
what the others were (or were not) doing. At least one
team - that led by Werner Heiscnberg, Nobel laureate
and dean of the Gentian physics community, who had
recently been appointed Director of the Kaiser
Wilhelm Institute at Dahlem - is reported to have
deliberately exploited the confusion which resulted to
drag its feet. Convinced that a bomb could be contructed,
Heisenberg set out to slow the process down,
and make as little actual progress as possible towards
its conclusion. Eventually, Albert Speer, Hitler's
Minister for Munitions, lost patience, and demanded
from Heisenberg a prediction of the length of time
which would be required to actually manufacture a
bomb. Heisenberg prevaricated still, but eventually
said that he believed it might be possible by 1945.
Speer decided to set up a single research project
charged with constructing a reactor. He assembled
some of the best brains in the field and asked them to
submit a budget. They requested 40,000 Rcichsmarks,
less than the cost of a single PzKpfw IV tank, and
this, more than anything, seems to have convinced
him that the project had a very low likelihood of success.
From then on, it seems, the nuclear research programme
concentrated on producing a reactor suitable
for power generation, rather than one to produce fissionable
material for a bomb. Naturally, such a power
station would inevitably produce small quantities of
fissionable material as a by-product, but it would be a
very long time before it would be possible to build a
bomb, even if the reactor worked perfectly.
Two atomic piles were eventually built, one near
Hechingen, the other near Erfurt, both using deutrium
as their moderator. Neither actually achieved a chain
reaction, largely because they were too small. By that
time - late 1944 - the infrastructure of German industry
was becoming increasingly chaotic. Such small
supplies of uranium ore as were available - from a
small field in Belgium and another in Bohemia - were
running low, and thanks to a successful bombing raid
by the RAE on the deutrium production plant in
Norway, that was in short supply too. The programme
was already dead in its infancy, and one might even
say that it was stillborn.
There was perhaps a subsidiary use of uranium as
a weapon of war under consideration. In 1943, HWA
commissioned a report from a biological laboratory
on the toxicity of radioactive material. From this it
has been widely concluded that uranium dust was to
have been employed as cargo in a conventional highexplosive
bomb or rocket warhead, but there is no
firm evidence to support this speculation and certainly
no evidence to suggest that even the most basic
experimentation ever took place outside the laboratory.
One could just as well conclude that the project
was aimed at improving worker safety.
BIOLOGICAL WEAPONS
Outside very special limits, suicidal attacks make little
tactical sense, and a suicidal strategy makes none
at all. Those truisms have always done more than pure
ethics or morality to control the use of one of the most
dreadful potential weapons known to man: disease.
Indeed, in limited 'experiments', where the vectors of
the disease in question could be completely controlled,
man has shown himself willing to use biological
agents of death. The US Army used it in the form
of smallpox-infected blankets distributed to native
Americans, and the Japanese did too in Manchuria in
the 1930s. But as an everyday weapon of war, it had
one enormous disadvantage: it was as likely to kill
you, in the long run, as it was to kill your enemy. That
is not to say that every country did not have its biological
warfare research establishments, but more to
suggest that much of the research carried out in them
was aimed more at providing a defence against the
agents of disease. There are persistent reports that
tests of biological agents were carried out on unwill-
Left: Like all armies, the Wehrmacht took chemical
weapons very seriously, as the protective clothing and
warning signs on this locker indicate.

ing participants in concentration and extermination
camps in Germany, and in the light of other undeniable
findings from the people investigating the events
in those places, we have to leave the question open.
CHEMICAL WEAPONS
More than half a century on, there is no lessening of
the revulsion felt against the obscenities committed in
the Nazi death camps or against the men and women
who actually committed the acts, and that is as it
should be. But besides the ethical and moral aspects,
there is also the purely practical to be considered, for
the destruction of six million or more people could
only proceed on an industrial scale. The mass murders
had to carried out under factory conditions. Very soon
it became obvious that the only acceptable method
would be by mass poisoning, the toxin to be delivered
in the form of a gas. In the event, this murder of millions
of helpless people was to be the only widespread
use of chemical warfare during World War II. This is
apart from Italian forces using phosgene in Abyssinia
in 1938, the Japanese use of it in China from the mid-
1930s to the end of 1941 in some 840 separate incidents,
and reports that something described as 'toxic
smoke' was used during the siege of Sebastopol.
German troops initiated the use of gas as a weapon
of war in February 1915, when they fired shells filled
with xylyl bromide (a lachrymogen, or tear gas)
against Russian forces. The operation failed, for the
gas was frozen solid in the shells, and dispersed only
very slowly. Two months later, they used chlorine gas
against British and Empire troops at Ypres with
greater success, and from then on it became a recognised
part of both sides' armouries. But it was not that
effective; gas was responsible for only just over one
per cent of battlefield deaths during the entire war. It
was slightly more effective as a wounding agent -
5.69 per cent of all injuries were caused by gas - and
from a military point of view, wounding is actually
more desirable, since caring for wounded both on and
off the battlefield eats into precious resources.
By 1919, there was a limited repertoire of gases
available; chlorine, mustard gas, phosgene and a few
others. By the time two decades had passed, there was
a whole menu of more effective agents available,
including some very exotic compounds which had
been produced during research into insecticides and
herbicides. These compounds were organo-phosphates,
and were to become the basis for what we now
call nerve gases. The original nerve gas, known as
Tabun, was first synthesised in 1936 into a substance
NUCLEAR, BIOLOGICAL AND CHEMICAL WEAPONS
Above: The sinister facade of a German mustard gas
storage building, in which the agent was kept in huge
concrete vats.
called ethyl-dimethyl-amido-phosphor-cyanidate. By
1942, a factory to produce it to the tune of 1016
tonnes f 1000 tons) per month had been established at
Dyhernfurth in Silesia (now Brzeg Dolny in Poland).
In 1938, a second and even more effective organophosphate,
isopropyl methyl-phosphoro-fluoridate,
was synthesised. Known as Sarin, it proved to be very
much harder to manufacture on an industrial scale
than Tabun, and even by 1945, only a small pilot plant
had been set up. By that time, a still more dangerous
derivative, pinacolyl methyl-phosphoro-fluoridate
had been produced, under the name Soman, though
little progress had been made with this by 1945.
It appears that until the factory producing Tabun
was overrun by the Red Army in early 1945, the
Allies knew nothing of these 'weapons', making their
existence one of the best-kept German secrets of
World War II. The first the British and Americans
knew came from examining shells and bombs recovered
from ammunition dumps (about half a million
shells and 100,000 bombs, in all), and as the reality of
the situation sank in, the researchers were horrified to
discover that they were confronted by a lethal agent,
and that there was no known cure or antidote from
exposure to it. That last factor, it is argued by many,
was the real reason that Germany did not employ
nerve gas, even in the final days. The Wehrmacht and
the SS could not be sure that the enemy did not also
possess these simple and cheap weapons of mass
destruction, and that the destruction which would
result from their use would not be mutually assured.
1 41

Page numbers in italics refer to picture
captions.
A-Stoff 72, 88
Achgelis, Gerd 54
'Adam' howitzer 114
'Aggregat'rockets 71-83
A2 73
A3 73
A4 see V2 ballistic missile
A5 73^,75
A6-AIO 82-3
air-to-air weapons 85-9
aircraft
gliders 41-3,45-8,55-6
hybrid and composite 49-51
jet 9-33
rocket-powered 35^3
rotary-wing 53-9
tail-sitting 57
see also air-to-air weapons
'Amerikabomber' 30, 33
anti-tank (AT) weapons /2/, 124-7
Antwerp, missile attack on 68, 81, 83
Antz, Hans 12
'Anzio Annie' 114
Arado, Ar 234 'BlitzTHechl' 17-19,
21
Argus pulse-jet engines 62, 63
artillery 109-19
autogiros 53, 54, 56, 58
B-17 Flying Fortress 49, 77, 85
B-29 Superfortress 25
Ba 349 'Natter' ,?5, 39-41,43, 86
Bachcm, Erich 39
Ba/ooka, copied 726, 127
Becker, Karl 71
BellX-5 25
'Biber' submarine 729, 136, 137
'Big Bertha' 110-11
biological weapons 140-1
Blitzkrieg 111
Blohm & Voss
Bv40 41,43
Bv 143 97,97
Bv 246 'Hagelkorn' 97
P. 212 26
Bode, Karl 54,55
Boeing-Vertol, V-22 Osprey 57
bombs see flying bombs; missiles,
air-to-surface
Br-StolT 102
Brandt, Edgar 116
Braun, Wernher von 36,63,72,73,
74,77,82, 105
Brest-Litovsk, Siege of (1941) 114
42
Index
Bulge, Battle of the (1944) 118
Buzzbomb see. VI flying bomb
C-Stoff 38
chemical weapons 139, 140, 141
chlorine gas 141
Cierva, Juan de la 53
Cierva, C.I9 54
'cross-Channel'guns 775, 116-17
Crossbow, Operation 77
'Deichselschlepp'system 41
Delta III 'Wespe' 37
Delta IV 37
DPS 39 37
DFS 194 37
DFS228 46
DFS 230 45-6
DFS 331 46
DFS 346 46
Dittmar, Heini 37-8
Doblhoff, Friedrich von 59
DoblhotTAVNF 342 59
Dönitz, Karl 129
Doodlebug see VI flying bomb
'Dora' gun 111-13
Dornberger, Walter 71, 72, 73, 75, 77
Dornier, Claudius 26-7
Dornier
Do 19 28
Do 217 95, 98
Do 335 'Pfeil'/'Ameisenbär' 26, 27
Douglas C-47/DC-3 19
Düsenkanone 280 29
EIOO 124
Eben-Emael 45-6,56, 126
Egret, HMS 96
Eisenhammer, Operation 51
'Electro-boats' 132-3
Emergency Fighter Competition/
Programme 24-6, 28
EMW
'Taifun' 107
'Wasserfall' 101, 105-6, 707
'Ente' aircraft 36
'Eve' howitzer 114
extermination camps 141
Federapparal-Torpedo 131
Fiedler, Willy 64
Fieseler, Gerhard 37
Fi eseler
Fi 156 'Storch' 39
Fi 103 see VI flying bomb
fin-stabilised, discarding sabots
(FSDSs) 116
Flak Rakete l 103
Flettner, Anton 57-8, 59
Flettner
FI 282 'Kolibri' 53, 57, 58-9
FI 184 58
FI 185 58
F1265 58
FI 339 59
flying bombs
Japanese 69
see also VI flying bomb
Focke, Karl 54
Focke Achgelis
Fa 61 53,54
Fa 225 55-6
Fa 266 'Hornisse'/Fa 223 'Drache'
54-5
Fa 269 56-7
Fa 284 57
Fa 330 'Bachstelze' 56
Focke-Wulf
FW 190 30,71,87
FW 190A-8 57
FW 190A-8/R2 39
FW 200 'Condor' 30, 94
Ta 183 25,30
Ta400 30
Triebfliigel' 57
'fortress smashers 1 113
'Foxer' 130
'Frilz-X' see Ruhrstahl, X-1
FSDSs (fin-stabilised, discarding
sabots) 116
FX ]400tt?eRuhrstahI,X-l
FZG76 83
Galland, Adolf 14, 16,85
Georgii, Walter 37
Gerät 041 'Karl' 113-14
Gerät 104 29, 87
Gerät 'MunchhauseiT 87
'Gerät-Schlinge' 43
Gerlich, Hermann 125
Gersenhauer, Helmut 55
girogliders 56
girokitcs 56
gliders 41-3,45-8,55-6
Gloster
E.28/39 11, 15
'Meteor' 64
'Goliath' tank 7
Goring, Hermann 9
Gosslau, Fritz 63
Gotha
Go 229 31,32,33
Go 242/244 48
Graf Zeppelin (ship) 134

grenade launchers 126,121
GT 1200 99
Günter, Siegfried and Walter 10
'Gustav'gun 77'0, 111-13
Hahn, Max 10
Hahn, Otto 139
'Hai' submarine 137
'Hccht' submarine 136
Heereswaffenamt (HWA) HI, 118
Heinkel, Ernst 10
Heinkel
He 70 10
He 111 10,68
He 111Z'Zwilling' 47
He 162 'SpatzTSalamander' 9, 12,
13,22-4
He 176 10,35-6
He 177 'Greif 28,29,87
He I77A-5 139
He 178 10-11,35
He 274 29
He 277 29
He 280 11-12, 14
P. 1077 'Julia 1 41
P. 1078C 26
Heisenberg, Werner 140
helicopters see rotary-wing aircraft
Henschel 27-8
Hs 117 'Schmetterling' 88,99,
101-3
Hs 132 28
Hs 135 28
Hs217 'Föhn' 40
Hs 293 28, 85, 88, 93-7, 99
Hs294 91,98,99
Hs 298 29, 88, 99
Hertel, Heinrich 26, 33, 48
HFB 320 'Hansa' 22
'High-pressure Pump' 111-19
Himmler, Heinrich 82
Hirth, Hellmuth 10
Hitler, Adolf 7
and aircraft 14-15
and artillery development 1 1 1
and the missile programmes 75, 77,
107
and submarines 129
and tank development 122
Hochdruckpumpe ('High-pressure
Pump') 117-/9
Horten, Walter and Reimar 31-3
Horten
Ho II 31
Ho VIII 32
Ho IX 31, 32, 33
P. 18 33
HWA (Heereswaffenamt) 111, 118
ICBMs 82
II Gruppe/Kampfgeschwader 100
(IT/KG 100) 95-6
III Gruppe/Kampfgeschwader 100
(ITT/KG 100) 92
ltd! U i (ship) 93
'Jagdverband T 16
Janus, HMS 93
Japan, suicide missiles 69,71
Junkers
Ju 88 87
Ju 88A-4 49, 50, 51
Ju 88G 20, 51
Ju 89/Ju 90 28
Ju248 39
Ju287 6, 19-22,33
Ju288C 28-9
Ju 290 30, 47
Ju322 'Mammut' 33,48
Ju388 29
Ju390 30
P. 128 26
P. 130/P. 140 33
K3gun 115
K4gun 115
K5 gun 109, 114-16
K12gun 116-17
Kamikaze campaign 71
Kehl/Strassburg guidance system 102
Kensche, Heinz 71
King Tiger (SdKf/ 182 Tiger II) tank
122, 123
Kneymeyer, Siegfried 20, 25
'Kommando Lange 1 7l
Kosin. Rüdinger 19
Kramer, Max 88
Kriegsmarine 58,59, 129
Krupp, Friedrich Alfred 111
Krupp, Gustav 111
KwK36 124
Lagenunabhängiger-Torpedo 131
Leyte Gulf, Battle of 71
Liege 110
Lippisch, Alexander 31,36-7
'Loki' howitzer 114
London
artillery to fire at 118
hit by flying bombs 68
and the V2 missile 80-1, £3
Ludendorff Bridge 17-19
Luftwaffe 9,30, 129
Lusser, Robert 12, 64
Lvov 114
M-Stoff 72, 88
machine guns, aircraft-mounted
MaginotLine 110, 111, 112
'Marder' submarine 135, 136
Mark 27 torpedo 131
Manch, Hans 12
5-7
NDEX
'Maus'tank 122-3, 124
"Meillerwagen' 77-9
Messerschmitt
Bf 109F 49,50,51
Bf 110 87
'Enzian 1 101
Me 163 'Komet' 26, 35, 36, 37-9
Me 262 'SchwafbeTSturmvogel' 9,
11, 12-17,86
Me 263 39
Me 264 29, 30
Me 321 'Gigant' 40,47-8
Me 323 'Gigant' 47-8
Me 328 29,41-3,71
Me 410 87
P. 1107 30
P. I 110 and P. III! 25-6
mines, submarine-launched 131
missiles
air-to-surface 91-9
inter-continental ballistic (ICBMs)
82
surface-to-air 101-7
surface-to-surface 61-83
see also air-to-air weapons
Mistel arrangement 41,45,49-51
'Mittelwerke' underground factory 69,
77
'Molch'submarine 135, 136
Mueller, Max 11
Multhopp, Hans 25
'Münchausen 1 cannon 87
Mussolini, Benito 46, 55
mustard gas 139, 141
'Neger 1 submarine 136
nerve gases 141
New York, possibility of bombing 30,
81
nuclear weapons 139—40
Oberth, Hermann 71, 72
'Odin' howil/er 114
Ohain, Joachim Pabst von 10, 11
Opel, Fritz von 36, 72
organo-phosphates, and nerve gas 141
P-Plane see V I flying bomb
PaK36 124
PaK41 125
PaK44 125
Panzer'Maus' 122-3, 724
Panzerbüchse 4l 125
Panzerfaust 30 726, 727
Panzerjäger Tiger 727,122
Panzerkampfwagen
PzKpfw IV 69
PzKpfw V Panther 7, 124
PzKpfw VI Tiger 7, 121-2, 123
'Panzerschreck' 727, 726, 127
Paris, and the V2 missile 80

INDEX
Paris Guns 109-10
Tarsival 1 guidance system 102
PC I400X see Ruhrstahl, X-1
Teenemünde arrow shell'
(Peenemünde Pfeilgeschoss) 113
Peenemiinde research station 72, 73,
74,77, 106, 107
Pfeilgeschossen 115-16
Philadelphia, USS 93
phosgene 141
Porsche, Ferdinand 727, 122
Puff, Karl 124-5
pulse-jet engines 62-3
R4M 40, 87-K
R-Stoff 102
radio-guided missiles 92
Raketenpanzerbüchse, RPzB
'Panzerschreck' I2I, 126, 127
Raketenwerfer 43 'Püppchen' 125
ramming tactics (Selbstopfermänner
fighters) 39-43
RAPs (rocket-assisted projectiles) 115
'RATO' (Rocket-Assisted Take-Off)
units 12
'Reichenberg', Project 71
Reichenberg IV 38, 69, 7 \
Reichsluftfahrtininisteriwn (RLM) 9,
30, 63^
Reichsverteidigungs programme 21
Reitsch, Hanna 31-2,39,41-3,53,
54,71
'Rheinbote' rockets 83
Rheinmetall, Gerät 041 'Karl' 113-14
Rheininetall-Borsig
'Feuerlilie' 104-5
'Hecht' 104
'Rheintochter' 105, 106
Rhön-Rossitten-Gesellschaft 45
Rh.Z.61/9 'Rheinbote' missile 83
rifles
anti-tank 125
recoilless 86
rifling, in artillery pieces 109, 114
RLM see Reichsluftfahrtministerium
rocketry
air-to-air weapons 87-8
aircraft 35^3
grenade launchers 726, 127
rocket-assisted projectiles (RAPs)
115
surface-to-surface missiles 61-83
Roma (ship) 92-3
rotary-wing aircraft 53-9
Rudat, Horst 50
Ruhrstahl
X-1 ('Fritz-X'; FX 1400) 28, 88,
91-3
X-4 29,88-9,91
X-7 'Rottkäppchen' 88, 127
144
Salbei 107
SAMs (surface-to-air missiles) 101-7
Sarin 141
Savannah, USS 93
Scapa Flow 50, 51, 87
Schlep, Helmut 12
Schlieffen Plan 110
'Schmetterling'missiles 88,99, 101-3
Schinetz, Heinrich 92
Schmidt, Paul 62, 63
schnorkels 134, 135-6
Scbastopol 112, 114
'Seehund' submarine 137
Selbstopfermänner fighters 39-43, 71
Sherman tank 124
Sikorsky, Igor 54
Skorzcny, Otto 46, 55
Soman 141
Sombold, So 334 'Rammschussjäger'
41
Sonderkommando 9 design studio 32
Sonderkornmando Elbe 39
sound, flying at speed of 46
Spanish Civil War 91
Spartan, HMS 93
Speer, Albert 117, 140
squeeze-bore guns 125
'Staffel Leonidas' 43,71
Slammer, Fritz 10, 36
Slrassman, Fritz 139
submarines 129, 131-4
firing A4 missiles from 81
girokites towed behind 56
midget 729, 136-7
schnorkels 134, 135-6
torpedoes and mines 129—31
suicide tactics 71
surface-to-air missiles (SAMs) 101-7
SV-Stoff 82. 102
'3x1000'bombers 30,32
T5 acoustic seeker 130
T-34tank 122, 124
T-Stoff 37, 38,66,77
Tabun 141
tail-sitting aircraft 57
tanks 7,69, 121-4
anti-tank weapons J21, 124-7
tapered-bore guns 124-5
tear gas 141
Thiel, Walter 75, 77
Thor'howitzer 1J3, 114
Tiger tank 7, 121-2, 725
TMA (Torpedo-Ankertaumine) 131
TMBandTMC 131
'Tonka' (fuel) 102
Torpedo-Ankertaumine (TMA) 131
torpedoes 129-31
air-launched 97-9
Troika-Schlepp' 46, 47
Type XVII U-boat 130, 131, 133
Type XXI U-boat 729, 132, 133, 134
Type XXIII U-boat 133-4
U-boats see submarines
Udet, Ernst 31
Uganda, HMS 93
United Kingdom
hit by flying bombs 68
and the V2 missile 80-1,5.?
United States, possibility of bombing
30, 33
Unternehmen Rumpelkammer 68
VI flying bomb (Fi 103) 62-70,74
manned version 38,61,69,11
V2 ballistic missile (A4 rocket) 61,
73,75,77-82,83
compared to 'Wasserfall' SAM
105-6
V80 submarine 131-2
Verdun 110
Versailles Treaty 6,71
Visol 82, 107
Vogt, Richard 26, 43
Voigt, Woldemar 13,25
Volksjäger (People's Fighter) 22^4
VTOL (Vertical Take-Off and Landing)
aircraft 57
Wagner, Herbert 88
'Wagner bars' 88, 102
Walter, Hellmuth I31-2
Walter RI-203 rocket 37
Warspite, HMS 93
Welter, Kurt 15
Wendel, Fritz 14
Weser-Flugzeugbau 56
Wiener Neustadler Flugzeugwerke
(WNF) 59
Wocke, Hans 19,22,33
Wulf, Georg 54
Wanderwaffen. 6-7
Wurfgranate (Spreng) 87
xylyl bromide 141
Yokosuka, MXY7 'Ohka' 69, 71
Z-Stoff 37, 66. 77
'Zaunkönig' acoustic seeker 130
Zeppelin 'Rammer' 41
Zindel, Ernst 33
'Zitterrochen' missile 99
'Ziu' howitzer 114
'Zossen' device 87